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This information is grouped into the following sections:
"RADAR" is a short form of the name "RAdio Detection And Ranging".
Basically:
- A radar set transmits radio waves out in a narrow beam (similar to a flash light beam).
- Some of the wave may hit an object and be reflected back (as an echo).
- Some of the echo is caught, amplified, and displayed by the radar set receiver.
- The time delay of the echo indicates the distance to the object.
The direction of the beam indicates the direction of the object.- The receiver displays the return signal on a display, with the echo as a bright spot or a raised blip.
An on-line Army manual "Introduction to Radar" ST-44-188-1 is available. There are two major types of radars, "pulse radar" and "continuous wave (Doppler) radar". (There is also a hybrid between the two sometimes called "Pulse-Doppler" used in Patriot radar. [thanks to Doyle Piland ])
(Also from Doyle Piland )
Chirp is another technology which is also used with pulsed radar. The general idea is to take advantage of the high power contained in a long pulse and still retain the range resolution of a short pulse. There are also other side advantages which makes it harder to use ECM against. Chirp simply uses a swept frequency, long pulse of up to 120 microseconds. I think the convention is the beginning of the pulse is the lower frequency and the high frequency is at the end of the pulse. When the return is received, the receiver delays different frequencies differently (called de-chirp). Thus, the energy contained in the return is compressed into a very short period of time, as if it were a short pulse. The Sentinel/Safeguard system made extensive use of "Chirp" techniques.As Nike radars (except HIPAR - which I do not know) used "pulse radar", we will discuss "pulse radar".
Short Powerful Pulses The "pulse" radar set sends out a very short (0.2 micro second to 1 microsecond) very high energy pulse of radar waves - then listens for echoes of this energy pulse. The pulse of radar waves needs to be as strong as practical so that the echo can be detected as far as practical. For Nike radars, the peak energy rate in the pulses ranged from 250 kilowatts for tracking radars to over 1 megawatt for the LOPAR acquisition radars. The average transmitted energy is much less because most of the time the wave is not being transmitted. (The average transmitted energy from most radars is about the same as a home microwave oven.)
Some search radars such as the Nike HIPAR, and the airborne AWACS search radar use much higher average and peak powers. The AWACS uses klystrons rated at over 50 megawatt peak power and over 50 kilowatt average power. HIPAR is reputed to have used similar technology.
Radar Echos are caused by many things, birds, planes, ocean waves, metal buildings, metal ships, some weather conditions, and so on. The pulses are short so that the echoes are short so you can more easily tell when the echo starts and stops from a particular object. If the pulse is long, and there are many objects, several objects could be echoing at the same time from the same pulse, making resolution between objects difficult or impossible.
Make a beam - like a long range flash light
Radar usually uses the shortest practical radio waves because short radio waves can be focused into a narrow "beam" with a smaller antenna than long radio waves. This is especially important in ship and airborne radars, but still important in all practical movable, steerable radars.
"Short" radio waves for radar usually are between 1 meter (300 million waves per second or 300 megahertz) and 3 centimeters (10,000 million waves per second or 10,000 megahertz or 10 gigahertz). Longer wave lengths than 1 meter require inconvenient sized antennas for anti-aircraft sites, and wave lengths shorter than 3 centimeter are increasingly hampered by weather and moisture in the air.
The focusing ability of a lens or mirror type antenna is directly related to its width in wavelengths of the radar wave. The wider the antenna is in wavelengths the smaller the angle of the beam that contains 50% of the radiated energy. The smaller the angle of the beam, the farther the radar can see the target and the more precisely the angle of the target can be known. Nike tracking radars had an effective antenna width of about 150 wavelengths. (The antennas were actually physically a little larger, but there are edge effects which decrease the focusing effect of the edge areas.)
Beam width - A rough (somewhat optimistic) formula for the beam width is
BeamWidthInDegrees = 57 * WaveLength / AntennaDiameter
where WaveLength and AntennaDiameter are in the same units.
A small (narrow) beam width in an acquisiton antenna is a "good thing", giving more more radar energy on the target (better range), and better target angle determination. An odd thing about an acquisiton antenna is that you often want to see all the targets at an azimuth regardless of target elevation (lets not worry about directly over head - it would be too late if a target got there). So frequently acquisiton antennas are wider than tall, giving a narrower azimuth beam width than elevation band width. This compromise permits better detection of targets regardless of their altitude.Nike tracking radars focused more than 50% of the radar pulse into a beam less than 1 degree wide, both horizontally and vertically. The acquisition radar beam was about 1 degree wide horizontally, but spread out vertically into a fan shape to see aircraft both near the horizon and also higher up.
Radar Range to any echoing object is measured by determining the delay between the transmitted pulse and the echo. The speed of a radar wave in air is about 300 meters per microsecond. (It varies very little with normal ranges of altitude and weather.) The round trip time for a radar pulse from transmitter to echo object to receiver is about 150 meters (164 yards). With electronics, measurement of the echo time to with in 5 meters is no technical challenge.
This Purcell interview mentions TR tube development, radar frequency troubles (water absorption line), and many other radar adventures.
One Antenna is used for both transmitting and receiving. This is actually rather tricky, as the transmitter sends a pulse of energy to the antenna sufficient to cook or spark most receiving components, then with in a few micro seconds, the transmitter must be electrically disconnected from the antenna and the receiver connected. This is microsecond switching function is performed in the radar "wave guide" by a "duplexer" circuit usually using a "TR" tube (transmit/receive tube). Basically, the powerful radar pulse causes an arc in the TR tube (in the wave guide), and the arc, being a conductor reflects most the pulse away from the receiver connection, keeping the pulse from the delicate receiver components.
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Download photo of a British TR tube
Wikipedia Cavity Magnetron, not available when much of the following was written.
Before 1939, radar waves were created using rather standard vacuum tubes. The tube shapes were changed to permit shorter wires (higher frequencies) but even the best technology was limited to pulses of about 2,000 watts at about 700 megahertz (700,000,000 waves per second). There was great desire to get higher frequency (for tighter beams with smaller antennas) and higher power (for longer range).In 1939, the British developed a remarkably simple method of generating an intense pulse of radar waves. This was the multi-cavity magnetron The arrival of the secret working British prototype magnetron into the U.S. caused great hope and excitement. The British prototype could deliver 10,000 watt pulses at 3,000 megahertz. This was 5 times the power (great!) at 4 times the frequency (wonderful!) of the best current technology. And the current technology seemed just about at its maximum (the components and systems had been pushed and tweaked extensively). And the newly developed magnetron from the British was just a research prototype - there could be room for big improvements.
This was a stunning "breakthrough". See "A History of Engineering and Science in the Bell System: National Service in War and Peace (1925-1975)" for further details. The British prototype was certainly improved in the U.S. for much higher power, manufacturability, stability, frequency adjustability and range, and other factors, but the impact of this basic invention on the successful Allied radar development was very great. It turns out that the mass manufacture of high performance magnetrons is much more tricky than first imagined. There were whole new worlds of large glass/metal seals, permanent high vacuum evacuation of machined metal castings, manufacturing tolerance of the cavity size and shape, cathode resistance to back bombardment, etc to be solved. Bell Labs and Western Electric made more than 100,000 magnetrons of various frequencies and powers for World War II.
This is another serious history on-line, local copy - about 1 megabyte .pdf - and an interview with Edward M Purcell
This "tube" helped guide the British fighter planes in the "Battle of Britain" bombings and gave the British (and the Americans) an advantage in the radar race until the Germans also developed one (from a downed British bomber?).
The 3,000 megahertz magnetron perfected from the British prototype had a very large (30 pound, 14 kg) magnet with a metal and glass "tube" about the size of a hockey puck (small can of tuna). (Higher frequency, shorter wavelength magnetrons and magnets are smaller and lighter.) It had a peak power of 1,000,000 watts (an improvement by a factor of 100). It was rugged and reliable.
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The above is a diagram of a magnetron (without output loop)
Notes : Not shown are two contacts for the cathode. These allow for cathode heater current (remember vacuum tubes had a hot part called the cathode to "boil off" electrons into the vacuum?). A special 5ish volt transformer was used which permitted the whole cathode to be at 18,000 volts during the short (about 1 microsecond) time the magnetron "fired". "Interesting" currents (about 100 amps) of the high voltage were required to generate 1,000,000 watts of peak power. Two get such currents emitted into the vacuum from the required small cathode, a coated cathode was used. This coating could be damaged more easily than the normal thoriated tungsten used in the usual high power tubes. The magnet and copper anode stayed at "ground" (zero volts).
Apparently the Brits were not the first to play with sloted magnetrons, but they were the first to use a loop the get the power out, this permitted
There were many interesting effects in the magnetrons (as in most of the other radar components). For instance, after the cathode was heated by the filament current, and the magnetron was pulsed with the high voltage pulses, there were so many electrons that would gain energy then come crashing back to the cathode that the cathode would over heat unless the cathode heater current was reduce or eliminated.
For a more detailed description of how a magnetron works, see The Magnetron Tube, Structure and Operation . This describes a microwave oven magnetron, which does not have the pulse width and tunability requirements of a radar magnetron, but the principle is identical.
For a detailed description of how a radar magnetron works, see Magnetrons.
And getting the power out of a magnetron, along with
- tuning the output over a 10% range - arcing - design variations such as "Amplitron"
can be "interesting".
The Modulator - A special circuit (modulator) would suddenly put a high voltage and current across the magnetron and out would come powerful radar waves. In the LOPAR acquisition radar, the modulator put about 18,000 volts at 100 amps for 1 microsecond through the hockey puck sized "tube" of the magnetron. The magnetron would put out about 1,000,000 watts of radar waves during this microsecond. This is repeated 500 times per second. - a nice trick - do that with your flashlight switch ;-))
This modulator tube took about 15 minutes to warm up properly. (Every thing else in the Nike system warmed up adequately in 5 minutes or less.) A 15 minute timer prevented the tube from being used during this warm up period. (There was a timer over-ride circuit so that it could be used sooner in a "battle emergency".) One night during the beginning of a routine alert, the captain got impatient waiting for this timer and activated the over-ride switch after about 10 minutes. The tube seemed to work just fine, the radar worked fine, nothing bad seemed to happen.
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A delay line helped limit the interval to 1 microsecond, and the operation with some diodes effectively doubled the source voltage of 10,000 volts ![]()
The Nike tracking radars had physically smaller (higher frequency) components with about 1/4 of the peak power (250,000 watts) and 1/5 the pulse width (0.18 microseconds).
For more on modulators, see the technical manual of a similar modulator Modulator and transmitter of the AN/TPS-1G ST-44-188-3G from Chuck Zellers - 2.5 megabytes
the Klystron another microwave source
In 1937, just before World War II, a device called a klystron was developed by the Varian brothers in California. In 1939 a handy form of "klystron" called a reflex klystron was developed in England by Robert Sutton.During World War II, the klystrons were primarily the reflex type and were used primarily as low power (milliwatt) oscillators in test equipment and radar and microwave receivers.
By the 1950's, there was a considerable demand for high power (kilowatt average power) microwaves, but with more precise control than could be generated by magnetrons. The customers were communications, medicine, science including particle accelerators, and radar. The Varian brothers, with the patents and the skills, did very well. Soon klystrons with average powers of 50 kilowatts and peak powers of 50 megawatts were available. To achieve the high current electron beam densities at these powers, powerful magnets (usually electromagnets) surround the tube. To get the most power from each electron in the beam, very high (100,000) voltages are typical.
These powers were impractical with magnetrons. The klystrons could deliver both the higher powers and also could amplify low level precise signals to these high powers. The klystrons were much larger (up to 2 meters long) and with their magnetic solenoids quite heavy (500 kilograms) and more expensive ($50,000), and more troublesome to keep running (required vacuum pumps) but they could be much more powerful and precise than magnetrons.
Power klystrons, such as described above have power gains (output signal/input signal) of over 10,000. As a comparison, typical power transistor in your stereo has a power gain of 20.
The Nike HIPAR radar transmitter used a
powerful klystron. 57 K Bytes. Image from Rolf Goerigk This one is about 5 feet tall 18 inches in diameter (including a focusing magnet - solenoid), and could output 10.4 megawatts peak pulse power - average power was 26 kilowatts. To help get that peak pulse power, 210,000 volts were used. This voltage gives much more powerful and numerous X-rays than your doctor's office machine - yes - the tube was surrounded by a lead shield.
The cooling system included 60 gallons of mixture of ethylene glycol and water (anti-freeze).
Yes - Lead Shield - There was a report that some technicians on the DEW line were tying to trouble-shoot a similar BIG klystron - and decided to remove the lead shielding for a while - If I remember the report correctly :-(( two of the technicians died with in two weeks of rediation "poisoning". I can't find the reference :-(( This class of tube does not sit happily in a glass tube and run unattended for years. The vacuum needed to be very high, and the klystron needed to be attached to a very good vacuum pump while in operation.
Because of possible rapid and precise changes of the frequency, amplitude, and phase of the output radar waves, very interesting receiver options are available to increase receiver efficiency (detect less reflective or further targets) and also to help suppress the effects of jamming (ECM).
Reflex klystrons were used as local low power ( 0.1 watt) microwave oscillators in many of the Nike radar receivers and test instruments.
Gary Evans asked if a "twystron" was used in the Nike system. I replied that I didn't think so - what is a "twystron"?
... AN/FSS-7 had a hybrid TWT/Klystron output device. The twystron was a big unit. stood about 4 foot tall , waveguide out direct to antenna system. Really seemed big for a freq in the 1-2 Gig range as I recall. Had a watercooling system. Ran a peak output of 4 Megs, but only a average of 7KW or so. (Short duty cycle - 20 microseconds transmit / 850 NM listen). Had a gigantic focus magnet around it (1000# or so) I seem to recall the Raytheon name on the side of the box it shipped in.
Wave guides (some times called "radar plumbing") are simple and complex at the same time. Radio waves can travel inside of a conductive (copper) pipe as long as the inside circumference of the pipe is longer than 1/2 of the wavelength of the radio wave. (Low frequency radars require larger wave guides.)
Radar waves can go through the convenient coaxial cables (similar to your cable TV lines). However there are several problems:
- Losses (attenuation) increase with frequency, and can get impractical at higher radar frequencies.
- Isolation between cables can get to be a problem.
- Peak power (related to maximum voltage) is quite limited.
Wave guides greatly reduce the above limitations and provide some interesting advantages:
- The greater conductivity of the greater surface of copper greatly reduces the resistivity and the air (or vacuum) in the cavity is a much less lossy dielectric than most available in coax cable.
- The thick solid walls are almost perfect isolators, preventing leakage into and out of the waveguide.
- The greater distance from wall to wall allows much higher voltages (and peak power).
- Various rotating, adding and subtracting tricks are much easier with wave guides.
For the above reasons, wave guides are very popular in radar units, even though they are more expensive and bulky and much less physically flexible. The cross section for the LOPAR antenna is about 1.5 inches by 3 inches (about 3.5 cm by 7 cm). The cross section for the X band tracking antennas is about 0.5 inches by 1 inches (about 13mm by 26mm). To provide better control of the various internal transmission modes, wave guides are usually constructed with a rectangular cross section. This limits some of the undesirable electrical modes possible in circular cross section wave guides.
All of the radars in the Nike system used wave guides. Almost all of the radars you have ever seen use wave guides. (The little radar receivers used to detect police speed radar "guns" use other methods.)
Most large acquisition radars have the magnetron in a fixed location. How do you get the radar waves from the fixed wave guide to the rotating wave guide if the radar "dish" is going round and round, and the magnetron is sitting in a fixed place?
A very practical question. The answer is a rotating microwave joint. At the center of rotation, the rectangular wave guide merges into a circular wave guide. The circular wave guide forms the center of the rotation. There is a trick used so that the copper of the rotating part does not need to touch the copper of the fixed part. Up in the rotating part of the antenna, the circular waveguide converts again to a rectangular wave guide and on to the feed horn (the part that lets the radar waves out into the air - or back again into the wave guide).For various reasons, Nike tracking radars have the magnetrons and receivers in the rotating part of the antenna. Later when we discuss "How The Tracking Radar Points at an Object", these rectangular wave guides will split the energy from the feed horns, rotate the waves, combine the waves in a subtractive way, do some more electronic tricks, and get antenna pointing error information. Just like magic.
Return to beginning of Nike Radars
Most radios (including your AM/FM, TV, cellular phone, and radar set) convert the received radio waves to a fixed frequency for amplification. This conversion is actually much simpler than trying to tune about 5 high gain stages through the desired frequency range. This group of about 5 high gain amplifier stages is formally called the Intermediate Frequency Amplifier or more commonly called the IF Amplifier. This technique saves many "big time" amplifier design, fabrication, and adjustment headaches.
The usual frequency in most radar sets for the IF Amplifier is about is about 30 megahertz (give or take 10 megahertz). To convert an example input radar signal of say 5,000 megahertz down to say 30 megahertz for the IF Amplifier you generate a signal 30 megahertz away from the input radar signal (in this case 5,030 megahertz is fine). The unit to make this extra frequency is called the "local oscillator" or "beat frequency oscillator".
Put this "local oscillator" signal, and the input radar signal together into a "mixer". The output of the mixer will contain all of the input frequencies plus the sum of the input frequencies (10,030 megahertz, which is not used) and the difference of the input frequencies (30 megahertz) which is amplified by the IF Amplifier.
The local oscillator at radar frequencies is usually a little reflex klystron .
The mixer can be a radio tube below about 1,000 megahertz, but above this frequency the radio tube is too inefficient and noisy. A "crystal" mixer was used in almost all of the radar sets during the 1940s and 1950s, (and is still in common use today in many commercial radar sets). (During the 1960s, a "traveling wave" tube was developed which could be made to have even lower noise than the crystal mixer. This is used in some demanding military, space, and research receivers, and was used in the Nike HIPAR radar receiver.)
So - in 1939 the invention of the magnetron permitted reasonable radar above 1,000 megahertz, and reliable, rugged crystal mixers were developed as low noise mixers to handle this higher frequency range. The research at Bell Labs that helped create those crystal mixers led directly to the invention by Bell Labs of the transistor a few years after the war and to the continuing semiconductor revolution and to your computer.
We adjusted the local oscillator power going into the crystal to give a crystal current of about 2 milliamperes. Too little power gave lower mixer efficiency, too much power gave more local oscillator generated noise.
Radar receivers are very similar to your usual TV receiver, and in many ways simpler because we don't have to play such interesting games processing the audio and color video. So we will just consider the TV "front end" through to the beginning of the audio and video (throwing out about 3/4 of the TV electronics.
All of the components are similar in function, and most are almost interchangeable with a radar set. The big difference is the front end where the incoming frequency is much higher. We will see that we quickly reduce the frequency to TV IF (intermediate frequency) and any TV repair person can take it from there.
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Component
Nametypical
TVtypical
radar...
CommentTuned Circuit 60-500MHz 9000-10,000MHz reduce undesired frequencies Mixer a tube
or transistora crystal output difference between signal and oscillator Oscillator 87-527MHz 9030-10,030MHz produce "beat frequency" for mixer, could be a klystron Auto Freq Control same same (AFC) controls frequency of oscillator AFC gate tracks sync pulse tracks magnetron pulse track only transmitted signal IF strip 27 MHz . increase signal to desired voltage using single frequency . . 30 MHz (acquisition radar) this lower frequency reduces noise . . 60 MHz (tracking radar) higher frequency to increase range resolution Auto Gain Control same same control gain of IF strip Gain Gate tracks sync pulse tracks target control gain of desired object Detector same same convert intermediate freq to video More correctly, military radar receivers are somewhat different from your TV in internal details to increase ruggedness, testability, maintainability, and to reduce the effects of various forms of enemy jamming. The field is large and complex and is beyond our scope here.
HOWEVER - a related acquisition pulse radar receiver AN/TPS-1G Receiver System ST-44-188-4G from Chuck Zellers - 2.08 megabytes is on-line at this web site. :-))
Since the radar frequency is about 1/3 that of the Nike LOPAR acquisition radar, some of the technology is slightly different - such asbut the cross-training is simple and quick - such what/where are the components and where are the interlocks. A bit like the differences in repairing two different brands of automobiles or washing machines.
- local oscillator is a different tube
- co-axial cables are used more in the AN/TPS-1G than wave guides
Return to beginning of Nike Radars
We have described many of the interesting radar components above. If we could visit a radar component supermarket (close out sale today), we could select components and build our own radar. Actually millions of people assemble components for their IBM clone computers and survive about the same complexity. There is a big difference in size, weight, voltage and powerful microwave radiation hazard. The general schematic would be:
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The components and their uses are:
Component Comments Start_Pulse_Generator One pulse a few microseconds before each radar pulse Power Supply 18,000 volts, otherwise a bit boring Modulator Sends a powerful 1 micro second pulse to the magnetron Magnetron Makes powerful radar waves (for 1 micro second) TR Tube Keeps most of powerful radar waves out of the receiver Receiver Amplifies the returned radar waves, giving video Display Tube Shows the return radar waves/video to the operator (PPI) (A scope) Tracking Unit Helps follow the selected signal in range, azimuth, elevation I must apologize to designers of military radars who add many small enhancements to reduce the effects of enemy jamming (and accidental friendly jamming). These enhancements may include:
- funny looking fins to reduce antenna side lobes
- facilities to easy rapidly change radar frequencies
- facilities to quickly change number of radar pulses per second or skip pulses
- changes in receiver details to counter overloads
- changes in receiver details to automatically/manually reduce sensitivity to certain patterns of jamming,
- and this list could go on for a number of pages
And the above list is for magnetron oriented pulse radars. This is the usual radar for private use, boats and ships, etc. The klystron based radars are not so common outside of military and research (such as imaging asteroids) use. Anti-jamming using these radars can be even more can be even more exotic. Or you can WOW your neighbors and buy major Nike system components, see How to get Nike Parts? .
Acquisition Radar (the wide eyes)
The Acquisition Radar is a most interesting looking radar. It is large and has motion, going round and round. It is often called a "surveillance" radar, providing the slant range and azimuth (direction) of all the radar visible objects in the area 5 to 10 times a minute.
A tiny bit of radar history
Before the Brits let the US in on their secret radar transmitter breakthrough, the Cavity Magnetron, the Americans were making radar sets the conventional way - with specially designed rather high frequency, rather high power triodes.
While I was at Chicago (1954) we had (for a few months) a very senior (like going to be retired at that rank) 2nd Lt. The poor fellow likely would have made an adequate Warrant Officer - but a rather hopeless commissioned officer. He was really a Dilbert type nerd, fine technically, but ... :-(( He said he had tried to tune acquisition radar transmitters that were pre-magnetron. The final amplifier was a ring of special triodes, set in a physical circle. Tuning that big parallel arrangement was difficult and time consuming.) Our magnetrons (1954) were basically "plug and play" ;-))
In any case,- the Army had just installed an SCR 270 type radar on a Hawaiian mountain, :-)) - looking west, on Sunday, December 7, 1941 :-)) - The operators detected and tracked a large flight of inbound airplanes, :-)) - which later turned out to be a Japanese attack force :-(( - They reported their find to HQ, :-)) - which did not recognize the threat :-(( Here is a display at the Historical Electronics Museum near Ft. Meade, MD. A great place to visit! :-))
Intro ![]()
Track over the ocean ![]()
enlarged ![]()
over the island ![]()
Usually surveillance radars have a longer wavelength than the tracking radars, as minimum beam width is less important. In the case of Nike, the LOPAR surveillance radar had a wave length of 10 centimeters (about 3,000 megahertz). (The Nike tracking radars had a wavelength of 3 centimeters or less.)
Charles D. Carter asked the question
"What is the difference between a HIPAR, LOPAR and ABAR?"
from Chuck Zellers Aug. 2009, via Charles D. Carter
LOPAR is the low power acquisition radar used in every Nike Ajax/Hercules site. LOPAR was used to "acquire" a target. ABAR is the "Alternate Battery Acquisition Radar" (AN/FPS-75) is the military designation, which was used on many Nike sites as a low cost alternative to HIPAR. HIPAR or "high power" Alternate Battery Acquisition Radar" as a high power (transmitter). Both ABAR and HIPAR were used as an acquisition radar that passed targets, typically ones that LOPAR could not acquire because of distance, etc. The HIPAR surveillance radar had a wave length of 23 centimeters (L-band, about 1,300 megahertz) and an effective range against large high-flying non-stealth aircraft of about 200 miles. The HIPAR radar had a large control building. There was very sophisticated pulse generation, and multi-channel receivers with unique moving target indicators (MTI) and great deal of anti-jamming capability. It was made by General Electric.
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A Nike HIPAR radar antenna with out protective radome, image is 74 K Bytes
(Photo credit - page 303 "Jane's Radar and Electronic Warfare Systems", 18th edition.) There is information that this picture does not include: 1) an anti-jamming antenna at the top of the main antenna, 2) two small antennas on each side, 3) an IFF antenna.![]()
A Nike HIPAR FAN radar antenna , image is 53 K bytes.
(Photo credit Rolf Goerigk![]()
A Nike HIPAR radar antenna with protective radome, image is 60 K Bytes
(Photo credit - adapted from Bill Benson , benson@efdata.com)
Note that the HIPAR antenna is high on a pedestal. There are 2 main reasons,
1) have the high power beam safely above any near by personnel
2) to gain a little range over the curvature of the earth.
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Drawing of HIPAR Station image is 71 K Bytes
Image from Rolf GoerigkFrom Rolf Goerigk, Specification for the HIPAR include:
Polarization horizontal Antenna Gain CSC2 antenna = 34.8 dB = 3020 ("CSC2" stands for co-secant squared, a vertical pattern optimized for aircraft detection at low and high altitudes and ranges)
FAN antenna = 29 dB = 790Beamwidth 1.2 deg Azimuth at 3 dB
1.3 to 7.1 in elevation
FAN 1.35 deg at 3 dBVertical Coverage 0 to 60 deg., 46 km height, 425 km length Antenna Speed 6.6 and 10 RPM (Revolutions Per Minute) Azimuth Accuracy > 0.25 deg. Noise max. 6.5 dB (1005 deg. Kelvin) Reflector Dimensions height 6.3 m (20.6 ft.), width 13.11 m (43.0 ft.), 82.6 sq. m (900.9 sq. ft.) - BIG Pulse Width 6 microseconds RF Freq Range 1350 - 1450 MHz (10 channels) RF Power: nominal: 10.4 MW / 26 kW average For a more detailed description of HIPAR, see Lesson 3. HIPAR Acquisition Radar - 1.7 megabytes
The HIPAR radar was very expensive, and was only used at selected Hercules sites. The other Hercules sites had "Alternate Battery Acquisition Radar"(ABAR) radar which was not so sophisticated, not so long range, and not so expensive. There were three models called "ABAR", the models were identified as AN/FPS-69, 71, and 75.
A catalog description of the AN/FPS-71 included the following phrases:
- 40 ft. reflector
- Frequency: 1220 to 1350 mHz
- Range, Max: 200 naut. mi, Min: 300 yd.
- Peak Power Output: 5 Mw, Pulse Width: 2 us, Pulse Rate: 325 to 400 pps.
- Peak Power Handling Capacity: 2 megw at .001 duty cycle
- Horizontal Beam Width: 1.4 deg. at half power points
- Vertical Beam Width: 6.2 deg. at half power points
- Special Features: Antijamming circuit that limits width of echo pulse that receiver will pass.
Peter DeMarco wrote about the AN/FPS-75
The ABAR we had in Alaska was the AN/FPS-75. I can't compare it to HIPAR but it had a range of about 200 miles and the ECCM equipment on it was very sophisticated. There were 6 different radar presentations I could view at the same time. Lots of buttons and lights. Chuck Zellers wrote about the generations leading to the AN/FPS-75 ABAR radar
I had written about lots of AN/TPS-1D (Tipsy Dogs) at Ft Bliss in 1954.May, 2008, Chuck adds ;-))
There a few differences between the AN/TPS-1G and the AN/FPS-36. The large schematics and one of the ST-44-188 manuals describe such differences. [See manuals.] The family of radars these systems belong to include the AN/TPS-1D (called tipsy dog). The AN/FPS-36 is a fixed radar system whereas the TPS series are transportable, hence the TPS designator. The FPS is the "fixed," non transportable designator. The FPS-36 has a much larger antenna (40'x11'), a pulse generator to generate a lower PRF, pulse repetition frequency. This allows the max range for the -36 to 200 nautical miles as opposed to the 160 NM for the AN/TPS-1G. The 36 receiver is also enhanced with a better signal to noise ratio. The receiver/transmitter and azimuth-range indicator are changed to allow the 200 NM range. The -36 uses a waveguide as opposed to the large coaxial cable used by the 1G.
The AN/FPS-75 is an AN/FPS/36 that is interfaced with the LOPAR PPI to allow ABAR video sweep presentation on the Acq PPI.
Many of the components from each system are interchangeable.
Googling "5J26" which is the magnetron used in the AN/TPS-1D/G and AN/FPS-36/75 ABAR radars provides additional info on the subject. Interesting and you can even purchase a 5J25 for a cool $3500.00!
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LOPAR Radar Photo credit, the Greek magazine "Modern Air Force & Navy", April 1998, Leonidas Blaveris (Nike articles by Pericles Zorzovilis) (49 K bytes)
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More details
- Auxiliary antenna [anti-jamming]
- Acquisition antenna
- Acquisition receiver-transmitter
- Acquisition modulator
- Acquisition antenna pedestal [drive motors, slip rings]
The LOPAR radar was very much like the original Nike Ajax (and M-33 gun) acquisition radar but with reduced pulses per second to match the longer range HIPAR radar or the ABAR radars mentioned above. It provided another "eye to the sky" and another problem for enemy jammers.
From Rolf Goerigk for the LOPAR include:
Polarization horizontal Antenna Gain CSC2 = 32 dB = 1600 ("CSC2" stands for co-secant squared, a vertical pattern optimized for aircraft detection at low and high altitudes and ranges) Beam Angle 1.4 deg Azimuth
2 to 22 deg. ElevationAntenna Speed 5, 10 and 15 RPM (Revolutions Per Minute) Azimuth Accuracy 1 deg. Noise 7.5 dB (1341 deg. Kelvin) Overall Noise 8 - 9 dB (1540-2014 deg. Kelvin) RF Freq. Range: 3.1 - 3.4 GHz RF Power average 650 W, peak 1 MW Pulse Width 1.3 microseconds Band Width IF = 4 MHz, Video=2 MHz Reflector Dimensions height 1.32 m, width 4.57 m, 5.6 sq. m For a more detailed description, see Lesson 2. LOPAR Acquisition Radar - 2.7 megabytes
From Rolf Goerigk "As I first worked on site (1961). I was able to change the elevation by operating the ELEVATION switch on the ACQ control console and some hydraulic control under the ACQ-RADOM. During the early 60s the control was modified to electromechanical. It was possible to change elevation between 0 to 391 mils and to change the elevation mode too. Actually controlled was the point in mils when the cosecant-rods were driven in or out the lower part of the reflector, i.e. changing from pencil beam (long range) to cosecant (great height)."
Acquisition Radar Displays, MTI, and Identification Friend or Foe (IFF)
The "ground clutter" shown on the above display can be a real problem in
some cases. The radar is sensitive to buildings, vehicles, mountains, trees, ...
for miles around. (For simplicity, the image above shows a trivial case.)
To aid in suppressing the ground clutter and enhancing moving objects (airplanes)
a system called Moving Target Indicator was developed. This indeed worked/works
quite well in emphasizing airplanes and reducing the interference in viewing them
due to stationary objects. The system could be switched ON and OFF
to present the best possible view of the situation.
For more than you will ever want to know about
Moving Target Indicator or MTI see
AN/TPS-1G Moving Target Indicator manual.
The LOPAR used a similar system.
The "IFF" (Identification Friend or Foe) is basically a series of coded pulses sent
out at the same time and same direction as the surveillance radar pulse.
It was sent out by separate IFF equipment. A "friendly" unit was equipped to respond to
the coded pulses with another set of coded pulses. These were received by the
IFF equipment, and usually displayed with the surveillance radar display.
The system resembles the methods FAA aircraft controllers use to track commercial
and other suitably equipped aircraft.
Enemy or accidental jamming can/will cause many other interesting
displays on the tracking scopes. Go to jamming for
more information.
The tube that turned on the pulse of current to the magnetron in the
LOPAR Acquisition Radar Modulator (see above) took up to 15 minutes to warm up
to operate reliably and not risk damage. There was a 15 minute timer to
prevent operation (with a switch to override the timer in case of emergency).
The operator has a number of controls, the following are of special interest:
"Also in your information on IFF, the Aradcom had two types of IFF. The
standard IFF had a limited set of codes and you used a code of the day.
Generally all freindlies used the same code. In 1963 we also adopted
SIF/IFF which allowed enough codes for individual identification of aircraft
or flights of aircraft. The IFF sent a pulse out a few microseconds after
the radar. The aircraft responded with its pulse code. This difference in
delay is why a second bar was painted above the aircraft on the screen. The
IFF/and SIF had a particular code sequence for emergencies. When the pilot
switched to that code, it automatically painted four bars which was Mayday."
I know about SIF/IFF because during a simulation with the Air
Force in 1963, we accidentally engaged a flight of USAF planes. This caused
a stir when it was found that we had SIF installed but were still using the
old IFF. So I was sent with two other technicians from Fort Heath to a USAF
Radar Site in North Truro, Mass where USAF personnel trained us on the SIF
equipment.
This site shows further
radar history Spotted by
Donald E. Bender.
Return to beginning of Nike Radar
Although the higher frequencies permit much smaller antennas to get the
same beam width, the higher frequencies suffer increasingly from
moisture in the air absorbing the radar waves. And also rain drops
reflect them more giving an effect similar to chaff. The choice of
radar frequency range for a particular application is a complicated compromise
involving many factors.
Got that? Clear as mud? Need a memory aid?
As a point of reference, the stealth fighter/bombers used in the Iraq conflict
are said by TV documentaries to have the radar reflectivity -"cross-section"- of a pigeon.
That seems an interesting accomplishment, as even one wheel of the aircraft
must have a much larger radar cross-section than a pigeon.
Accidental Jamming - Pulse Radars (used in Nike)
There are many friendly sources of radar interference.
Most folks worry about other friendly radars. However, these
are not a big problem at a typical Nike site, or even a
group of Nike sites very close together such as a Nike range at Red Canyon or McGreggor.
How can this be? Radars "shouting" all over the place,
and no problem? Unbelievable! But oddly enough, there is no big problem.
Here is why.
The attempt is not perfect, but usually about 95 % of the energy
gets directed as desired.
Nike radar magnatrons tune over a range of +- 5% from their center
frequency. And the receivers are tuned to be sensitive to roughly 0.1 % of that range.
In effect, about 500 radars in one band (+- 5% ) could be tracking one target
and not interfere with each other with respect to frequency.
Except - Nike site SF-59 was reported to be
jammed by the TV Channel 2 transmitter a half mile away.
Radar Jamming, Electronic Counter Measures (ECM)
The target may not wish to be observed, and/or may wish to reduce the
effectiveness of the radar attempting to observe it.
One way to reduce the effective range of the radar is to reduce the
reflectivity (ratio of energy reflected back) of the target.
This is called "stealth"
and is for aircraft designers, not us.
"Jamming" or "Electronic Counter Measures" (ECM) is a term used to describe
active means of trying to prevent the radar system from working as well as
intended. And of course radar designers actively try to defeat the ECM.
It is a great (but deadly) game of radar counter measures, counter-counter measures,
counter-counter-counter measures, played with very serious intent.
We will very briefly mention a few popular forms of
jamming:
From Peter De Marco
There are basically two types of radar jamming;
ECCM is an complex field and there are several operational and equipment techniques used by the ECCM Radar Operator to try to counter the jamming. The most important component of ECCM is the Radar Operator. The improper use of ECCM equipment and techniques can do more harm than good.
When the radar was being jammed there were several signal processing techniques that the ECCM Radar Operator could use to counter the jamming. Some of these methods are normally installed in radars to overcome natural phenomena such as weather or ground clutter, but they are all considered ECCM.
When the site was at Battle Stations or Blazing Skies it took two people to operate the ABAR equipment. One person was in the equipment room, which was located just below the radar dome. It was his job to keep the ABAR radar equipment peaked and running.
The other person operated the ECCM console, which was located in a room next to the Battery Control Van. It was his job to determine the type of ECM that was being used against the radar and to counter the effects of the jamming.
Since the range of the ABAR (about 200 nm) was greater than the LOPAR the ECCM Radar Operator would also call out targets that he was tracking to the Battery Control Van. The ABAR and the LOPAR were linked to the radar presentation in the Battery Control Van and the commander could switch from the LOPAR radar presentation to the ABAR radar presentation at his discretion.
The ECCM console could display six radar and two oscilloscope presentations at the same time. The main display showed what the ECCM Radar Operator considered the best radar presentation of the targets being tracked.
The other displays showed "previews" of the different types of ECCM presentations available. These ECCM presentations included "Dickie-Fix", "Side Lobe Blanking", "Slide Notch I-F Canceler", "Moving Target Indicator", etc.
By properly employing some or all of the above mentioned techniques the ECCM Radar Operator could significantly reduce the effects of ECM jamming.
For discussions of handling jamming in the Target Tracking Radars see:
Some of the nomenclature found by Don Bender include:
Impulsive noise, that can shock-excite the " narrow-band " radar receiver
and cause it to ring, can be reduced with the Lamb noise-silencing circuit,"
or Dicke fix." This consists of a wideband IF filter in cascade with a limiter,
followed by the normal IF matched filter. The wideband filter is designed
to include most of the spectrum of the interfering signal. Its purpose is to
preserve the short duration of the narrow impulsive spikes. These spikes
are then clipped by the limiter to remove a considerable portion of their energy.
If the large noise spikes are not limited and are allowed to pass they would
shock-excite the narrowband IF amplifier and produce an output pulse much
wider in duration than the input pulse. Therefore the interference would be in
the receiver for a much longer time and at a higher energy level than
when limited before narrowbanding. Desired signals which appear
simultaneously with the noise spike might not be detected, but the circuit
does not allow the noise to influence the receiver for a time longer than the
duration of a noise spike. This device depends on the use of a limiter. Limiters,
however, can generate undesired spurious responses and small-signal suppression,
and reduce the improvement factor that can be achieved in MTI
processors. It should therefore be used with caution as an ECCM device. 1f
incorporated in a radar, provision should be included for switching it
out of the receiver when it does more harm than good.
... Furthermore, at the higher frequencies the antenna sidelobe levels can be lower, making it
more difficult for sidelobe jamming. However, the advantages of operating against jammers at the higher
frequencies are balanced in part by the disadvantages of the higher frequencies, especially above L band,
for long-range air-surveillance radar.
The noise that enters the radar via the antenna sidelobes can be reduced by
coherent sidelobe cancelers. This consists of one or more omnidirectional antennas and cancellation circuitry
used in conjunction with the signal from the main radar antenna. Jamming noise in the omnidirectional
antennas is made to cancel the jamming noise entering the sidelobes of the main antenna." An antenna can also be
designed to have very low sidelobe levels to reduce the effect of sidelobe jamming. Low sidelobe antennas require
unobstructed siting if reflections from nearby objects are not to degrade the sidelobe levels.
By employing some or all of the above techniques, the effect of the sidelobe noisejammer can be significantly
reduced. Some of the above techniques can also reduce the jamming that enters via the main beam. The effects
of main-beam jamming can be further reduced by employing a narrow beamwidth to limit the region over which the
jamming appears. If the main beam cannot be made narrow because of constraints on the antenna size, an
auxiliary antenna can be employed to create a notch in the main-beam radiation pattern in the direction of the
jammer. With adaptive circuitry similar to that of the sidelobe canceler, this main-beam notch can be
automatically adjusted to be maintained in the direction of the jammer.
A web site involved with jamming is
EW Tutorial, Table of Contents
A book recommended by Aidan Fabius
via newsgroup sci.military.naval and Patrick Tufts
recommends
For further information, see "An Illustrated Guide To The
Techniques And Equipment Of Electronic Warfare"
There is a T1 manual on-line at
T1 AN/MPQ-T1
.pdf files - (7.5 Mbytes)
The information from surveillance radar is customarily displayed
with the "Plan Position Indicator"
tube, abbreviated to "PPI scope". This is the big round CRT (TV) tube with the
sweep going around all the time. Basically, you and the radar set are in the middle of this
big round map, and the radar us showing you what is going on around you.
50,000 yards (about 28 miles)
150,000 yards (about 85 miles)
250,000 yards (about 140 miles)
350,000 yards (about 200 miles)
Although some very long range radars (such as Nike HIPAR) were fixed at about 7 RPM
From Robert Noakes March, 2001
A PPI display with planes and jamming image is 35 K bytes.
(Photo credit Rolf Goerigk
There are various unverified stories that in practice combat between the
Air Force with their jamming equipment, and the Nike with their anti-jamming
equipment, that the Nike successfully tracked the Air Force planes and would
have had successful intercepts with the Hercules missiles.
This was reputed to be true even when the Air Force used their best jamming equipment
to try to confuse the tracking.
Radar History
The following is from "Radar Technology", edi. Eli Brookner,
(C) 1977 ARTECH HOUSE, INC. ISBN 0-89006-021-5
1886-1888 Heinrich Hertz demonstrates generation, reception,
and scattering of electromagnetic waves
1903-1904 Christian Hulmeyer develops and patents a primitive
form of collision avoidance radar for ships
1922 M.G. Marconi (in acceptance speech for an honor)
an angle-only radar for ship collision avoidance
1925 First short pulse echoes from the ionosphere are
observed on CRT by G. Breit and M. Tuve of
Johns Hopkins University
1934 First photo of short pulse echo from aircraft made
by R.M. Page of Navel Research Lab.
1935 First demonstration of short pulse range
measurements of aircraft targets, by British and Germans
1937 First operational radar built - the Chain Home in
Britain, designed by Sir Robert Watson-Watt
1938 Signal Corps SCR-268 becomes first operational
anti-aircraft fire control radar; 3100 sets eventually produced,
Range, > 100 mi.; freq, 200 MHz
1938 First operational shipboard radar, the XAF, aboard the
battleship USS New York, 12 mi ships, 85 mi aircraft
1941-Dec By this date, 100 SCR-270/271 Signal Corps early
warning radars have been produced. One of these radars,
located (near) Honolulu, detects Japanese planes approaching Pearl Harbor ...
Radar Frequency Bands
"Old style"
band naming convention
Wavelength in cm = 30,000 / frequency in MHz
Band
Frequency(MHz)
Wave Length
Comments & common usage
VHF
214- 236
130 cm
?
P
300
100 cm
?
UHF
425- 610
60 cm
BMEWS (ballistic early warn), PAVE PAWS
L
1250-1380
23 cm
Airport Surveillance, Nike HIPAR acquisition
.
1227.6 & 1575.42
about 20 cm
GPS (Global Positioning System)
.
1,421
21.11 cm
Hydrogen (Radio Astronomy)
and watched by SETI@home.
.
2,450
12 cm
(magnetron in your microwave oven)
S
2700-3900
10 cm
Sage, DEW line, Nike LOPAR acquisition
C
5300-5520
5 cm
Height Finder, Patriot
X
9230-9404
3 cm
Precision Approach, Nike Target Tracking (TTR)
Ku
16,000
18 mm
Nike Target Ranging Radar (TRR), Mortar-location
K
20,000
15 mm
?
.
22,000
13.6 mm
minor H2O absorption line
.
31,500
10.5 mm
(Cosmic Background - "Big Bang")
Ka
35,000
8.5 mm
nominal upper limit of traditional radar
Q
"millimeter"
40,000
7 mm
used in outer space
.
60,000
5 mm
major O2 absorption line, fog (clouds) becomes a major problem
Radio Frequency Naming Convention
Band
Frequency(MHz)
A 0 - 250
B 250 - 500
C 500 - 1000
D 1000 - 2000
E 2000 - 3000
F 3000 - 4000
G 4000 - 6000
H 6000 - 8000
I 8000 - 10000
J 10000 - 20000
K 20000 - 40000
L 40000 - 60000
M 60000 - 100000
Radio Frequency Naming Convention
Band
Designation EVLA
Frequency
Range (GHz)
4 73.5-74.5 MHz
P 300-340 MHz
L 1.0-2.0
S 2.0-4.0
C 4.0-8.0
X 8.0-12.0
Ku 12.0-18.0
K 18.0-26.5
Ka 26.5-40.0
Q 40.0-50.0
Range vs. Stealth
Notes on detectable range and "stealth" aircraft
(who wants his radar to spot aircraft as far away as practical)
Doubling the detectable range requires (all other things remaining the same)
increasing power by 16
target_radar_cross_section * radar_power * antenna_gain
/ range^2
reflected_power * antenna_gain / range^2
so
effective_radar_range ~ ((antenna_gain ^2) * radar_power) ^0.25
so
multiply original power by
increases range by
range, if original radar could see 64 miles
2 1.2 76
4 1.4 90
8 1.68 107
16 2.0 128
(who wants his aircraft to have low visibility to radar)
Pity the poor aircraft designer whose aircraft can be seen by a radar at 64 miles,
and is told to make the aircraft "invisible" a 4 miles.
or
reducing effective cross section by 16
So, to decrease the detection range of the aircraft by a factor of 16,
the designer/manufacturer has to decrease the reflectivity of the
aircraft by a factor of 65,536, likely to be a really major effort.
divide original reflectivity by
decreases range by
detection range, if originally 64 miles
2 1/1.2 53
4 1/1.4 46
8 1/1.68 38
16 1/2.0 32
256 1/4 16
4096 1/8 8
65536 1/16 4
Summation: Accidental jamming was not a significant problem in Nike sites,
even when located close together as in firing ranges.
AN/FPS-75 Alternate Battery Acquisition Radar (ABAR) & Electronic Counter Counter Measures (ECCM) Console from the point of view of the Radar Operator.
Some of the most popular types of jamming used by the ECM Specialist on enemy aircraft are:
The ECM Specialist on the aircraft and ECCM Radar Operator at the radar site play a type of electronic chess game. This game is played with very serious intent and can result in deadly consequences.
And thanks to Robert Noakes for nudging me into
further reading and quoting the above book sections.
[From the book Introduction to Radar Systems by Merrill L. Skolnik, 1980,
pages 549-550]
[From the book Introduction to Radar Systems by Merrill L. Skolnik, 1980,
page 549]
Patrick Tufts then found an almost local
(for me) copy the book
via Advanced Book Exchange.
... excellent book on the subject called "An Illustrated Guide To The
Techniques And Equipment Of Electronic Warfare" by Doug Richardson (An ARCO
Military Book) which has tons of info on that kind of thing. My copy is
pretty dated (1985) but there's probably a newer version of it by now.
There's about 20 pages on different jamming techniques and a really good
introduction explaining how radar works and all the different types of
radar. The book has plenty of pictures and diagrams, and is really easy to
understand. I highly recommend it."
and if that is not enough see
"Radar Electronic Counter-Countermeasures"
should provide more than enough.
The ability of a target aircraft to carry and launch a missile to follow down your radar beam to your radar (and you) was just a future possibility in 1956. To put a useful radar tracker into a missile small enough to be handy is an interesting design and production challenge.In principle the aircraft being illuminated by the radar permits one of the aircraft's ARM missiles to lock onto that radar, and the aircraft can then "launch and forget" the ARM missile. The illuminating radar may be able to see the very small "radar cross section" of the missile at closer ranges, especially if the missile is currently in the major lobe of the radar.
I understand that that ARMs were used successfully in the Gulf War, if not previously. Unfortunately, at the present time I know nothing about them.
And then Bill Cahill responded to the above:
The actual category of weapons is called ARMs (Antiradiation Missile) while the HARM (High Speed Antiradiation Missile) refers to a specific weapon, the AGM-88. ARMS were first used in the Vietnam War in Mar 1966 by Wild Weasel 1 (F-100F) aircraft carrying the AGM-45 Shrike, the first ARM in the US inventory. The Shrike, built by Texas Instruments, had different variants designed to home in on different frequencies. If the radar went off the air, the missile went stupid. The Shrike was essentially an air launched version of a semi-active radar homing surface to air missile, homing in on the target radar instead of a target illuminated by a host radar. Shrikes were effectively used by the US in Vietnam and Israel in the Middle East.
The AGM-78 Standard ARM augmented the Shrike in 1968, providing greater range and mission flexibility. The Standard was improved over the next 10 years, with many variants entering service with the USAF and USN. Unlike the Shrike, the Standards can 'remember' where a radar is even if it ceases transmission. The ultimate (to date) ARM, the HARM, entered service in the mid 1980s. This high speed, maneuverable missile is currently in inventory with the USAF and USN and has replaced the Shrike and Standard.
And then Nicholas Maude responded to the above:
I just read the update, at the bottom you assert that the HARM is the best ARM around ,that is only partly correct. You are correct if you saying it is the best American ARM around. The best ARM around is the British aerospace ALARM, not is it more modern, it is half the weight of a HARM and is flexible since if it does not immediately detect its target ,it climbs to 70000Ft and deploys a drogue shute. It can stay in this mode for 15 minutes, if detects the target during this period it cuts lose and literally drops in detonating when it is beside the target in a vertical dive.
Various groups use measurements of historical or practical significance. Examples are the jeweler's use the "carat" for weight and American's use of the old "English" system of measurements.U.S. Artillery also uses measurements of historical significance. These units were in use 40 years ago.
(*) Units that only scientists or engineers love.
unit S.I. (mks, metric) name an "English" name Artillery name length meter yard yard volume liter gallon gallon force newton(*) pound pound mass kilogram slug(*) . plane angle radian degree or radian(*) mil(**) (equals milliradian) time second second second temperature degree Celsius or Kelvin(*) degree Fahrenheit degree Fahrenheit
(**) The angle included by 1 unit at a range of 1000 units. 1 mil equals about 0.0573 degrees. This strange sounding unit is very handy in aiming and estimating errors in gun artillery and missiles. An azimuth error of 1 mil at a range of 25,000 yards is a miss by 25 yards. A tracking radar pointing error of 0.1 mils (0.00573 degrees) at range of 132,000 yards (75 miles) yields a "miss" of 13.2 yards. (A Nike warhead exploding 13 yards from a flying aircraft will instantly turn that aircraft into a falling pile of junk.)In 1997, I asked Col. Moeller - MoellerS@ssdch-usassdc.army.mil - if these units were still in use. He kindly responded as follows:
"The only change that I can see would be that we seldom use yards any more, but describe that unit of measure in terms of meters. That ties in with our use of military grid overlays on maps which are done in meters and kilometers. Altitude is still done in thousands of feet, just like commercial airliners use, "Ladies and gentlemen, our cruising altitude today will be 30,000 feet." Mils are still used in the artillery as a more precise measurement than degrees, although degrees are used also. We still use pounds and gallons for measurement."and "We us standard US weather lingo, definitely F, not C."
J.P.Moore found this:http://www.bts.gov/NTL/DOCS/3910-3a.html
If you have comments or suggestions, Send e-mail
to Ed Thelen
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Updated Sept 6, 2009