Flexible Lightweight Agile Guided Experiment (FLAGE)

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FLAGE (flexible lightweight agile guided experiment) - formerly known as SR-HIT (small radar-homing intercept technology) -- was the predecessor of the current Patriot PAC-3 ERINT interceptor. FLAGE was a small (9 inches in diameter) highly-maneuverable, millimeter-wave radar-guided interceptor intended for relatively short-range intercepts well within the atmosphere. The missile spins during flight and its center of gravity and center of pressure are reportedly very close together, making it inherently unstable. 216 small solid rocket motors mounted in the missile body forward of its center of gravity were used to achieve very high maneuverablity (reportedly about 100 Gs).

***January 20, 1984. First flight test. An unguided ballistic trajectory flight to test missile performance and stability. Reportedly a success. First of a planned series of nine flight tests.
***March 15, 1984. Second flight test. Non-homing test in which the missile was to make a series of six pre-programmed maneuvers. Missile became unstable during second maneuver, and its radome and fins were torn off. Prior to the third test, ballast was added to improve the missile's aerodynamic static margin.
***November 29, 1984. Third flight test. Non-homing test. The missile reportedly successfully executed a series of pre- planned maneuvers.
***Date?? Fourth flight test. Test was to be against a stationary target suspended from a balloon.
***April 20, 1986. Fifth flight test. Target was a 44 inch diameter aluminum sphere held in place at 12,000 feet (3.7 km) altitude by a balloon. Test was a success, with missile passing through the target.
***June 27, 1986. Sixth flight test. First intercept attempt against a simulated missile target, and the interceptor hit the target. The intercept took place 7 seconds after the interceptor launch at an altitude of about 12,000 feet (3.7 km). There was no up-link to interceptor after its launch. At intercept, FLAGE speed was 3,200 ft/sec (0.98 km/sec) and the target speed was 3,800 ft/sec (1.16 km/sec). The target was launched from an airplane and reportedly had an RCS of about 1 square meter. At the time of test, it was described as the sixth test in a series of nine.
***May 21, 1987. Seventh flight test, second intercept attempt. The FLAGE successfully intercepted a Lance ballistic missile (said to simulate a Soviet SS-21 missile). The Lance reportedly had a much smaller radar cross section than the previous targets. The intercept took place seven seconds after the FLAGE launch, at an altitude of 12,000 feet (3.7 km). At intercept, FLAGE speed was 3,200 ft/sec (0.98 km/sec) and the target speed was less than 3,000 ft/sec (0.91 km/sec). The FLAGE radar reportedly acquired the target 2 seconds before the intercept and 60 of the 216 small solid rocket motors were fired during the flight.

Following the seventh flight test, it was reported that a second flight against a Lance missiles would be attempted in July 1987, and that a third test might be conducted after the data from the first two tests against a Lance were analyzed. However, I have not found anything indicating that either test occurred.
 
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SRHIT -> FLAGE -> ERINT -> PAC-3

They also used it to shoot down this weird looking target vehicle. IIRC the target reached Mach 5.

F-4J_wilth_FLAGE_missile_in_flight_near_Holloman_AFB_1986.jpg

"With Holloman Air Force Base, New Mexico (USA), in the background, a U.S. Navy McDonnell F-4J Phantom II carries the target vehicle for the sixth flight of the U.S. Army's Flexible Lightweight Agile Guided Experiment (FLAGE) Project toward White Sands Missile Range, on 27 June 1986. After the target was released from the aircraft, its rocket motor ignited, boosted it to the required velocity, and separated. Approximately 30 seconds after release, the FLAGE vehicle, guided by its built-in active millimeter wave radar and unique steering rockets, hit and destroyed the target. This was the first moving target for the U.S. Army Strategic Defense Command Project, which was aimed at validating technologies for the Strategic Defense Initiative Program to provide sufficient confidence that guidance accuracy could be achieved permitting non-nuclear intercept of ballistic missile reentry vehicles within the atmosphere. "

DehgY0cV4AAVA4P.jpg
 
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formerly known as SR-HIT (small radar-homing intercept technology)

I suspect the word "Radar" was inserted at the insistence of some prude, against the will of a wiseacre who wanted to call it Small Homing Intercept Technology (with obvious consequences).
 
formerly known as SR-HIT (small radar-homing intercept technology)

I suspect the word "Radar" was inserted at the insistence of some prude, against the will of a wiseacre who wanted to call it Small Homing Intercept Technology (with obvious consequences).

Except that it does in fact use radar homing when virtually all other missile defense programs in the US at the time used IR.
 
formerly known as SR-HIT (small radar-homing intercept technology)

I suspect the word "Radar" was inserted at the insistence of some prude, against the will of a wiseacre who wanted to call it Small Homing Intercept Technology (with obvious consequences).

Except that it does in fact use radar homing when virtually all other missile defense programs in the US at the time used IR.

I don't doubt that it describes the reality. I'm saying it's quite feasible to leave the R out in order to stir one's superiors with the title of the technical brief (and then politely but firmly be ordered to put it back in again).

The Hawk missile also uses radar and stands for Homing All-the Way Killer. Radar is not mentioned, so as to give a pleasing acronym that's easy to say out loud.

SR-HIT could equally easily delete the R to create a (deliberately) displeasing one!
 
Wasn't the basis for the FLAGE airframe the M26 rocket used in the M270 MLRS?
 

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