Friday Fun Facts – 31st July 2026

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ASAT_missile_launch

On the 13th September, 1985, an F-15A launched an ASM-135 Air-Launched Anti-Satellite Multistage Missile, at an altitude of 11.6km, knocking out and destroying the Solwind P78-1 satellite, flying at an altitude of 555km.


ASM-135 ASAT

The ASM-135 ASAT was a missile born out of a project that was originally conceptualized back in the 1950’s, where the USA began development of anti-satellite weapons. The first one was the Bold Orion weapon system, which was tested in 1959, but failed.
Over 20 years later, the ASM-135 was finally built, based on a modified Boeing AGM-69 SRAM missile, with three stages involved.


The ASM – 135 was designed to be launched from an F-15A in a supersonic zoom climb.
It consisted of three stages.

  • Stage 1, had the modified AGM-69, with a solid propellent two pulse rocket motor.
  • Stage 2, used a Altair 3 solid rocket motor. It also included hydrazine fueled RCS thrusters that could be used to point the missile towards the target satellite.
  • Stage 3, consisted of a SRAM booster, and was called the Miniature Homing Vehicle Interceptor. Prior to the second stage being deployed, it would spin up to 30 RPM, and point it at the target.

F-15A

DAYTON, Ohio — McDonnell Douglas F-15A at the National Museum of the United States Air Force. (U.S. Air Force photo)

The F-15A

The F-15A was the first operational variant of the McDonnell Douglas F-15 Eagle. The F-15 was designed as the principal air superiority fighter of the US Air Force and several U.S. allies during the late cold war, replacing the F-4 Phantom II. 384 were built during the period of 1972-1979. With a combined engine thrust of 211.4kN, it was easily Mach 2 capable at altitude, with a range of 2,144 nautical miles. It would carry either 4x AIM-7 Sparrows & 4 AIM-9 Sidewinders or 6 AIM-120 AMRAAM & 2x AIM-9 Sidewinders.


Mission Profile

Following the authorization from Ronald Reagan to test against a satellite, a target, Solwind P78-1, which was a solar observatory, was chosen. On the 13th September, 1985, Wilbert Pearson, flying F-15A 76-0084, launched the ASM-135 about 320km west of Vandenberg AFB. Prior to the launch, the F-15, flying at speeds of Mach 1.22, executed a 3.8g0 (37m/s2) zoom climb at an angle of 65o. The ASAT was automatically launched at 11,600km, FL381, while the F-15 was flying at Mach 0.934. The final stage, the 14kg MHV, collided with the 910kg P78-1 satellite at a closing velocity of 24,000km/hr.

The Aftermath

Following the impact, NASA, working with the DoD, used two orbital debris telescopes, and a re-entry radar deployed in Alaska, to monitor the outcome. While they assumed the metal would be bright, the debris ended up being so dark, it was almost undetectable, and only 2 pieces were actively seen.


This was theorized to have been caused due to the carbonization of organic compounds inside the satellite, that when the kinetic energy of the ASAT became heat energy on impact, the plastics inside Solwind vaporised and condensed on the metal pieces as soot.


NASA used USAF infrared telescopes to show that the pieces were warm with heat absorbed from the sun. The pieces decayed quickly from orbit, implying a large area-to-mass ratio.

According to NASA, the last piece of debris had deorbited on the 9th May, 2004, named COSPAR 1979-017GX. There was 285 trackable pieces of debris, and by January 1998, only 8 had remained trackable, after 13 years.

The Solwind test had three important results.

  • It raised the possibility that optical identification systems were actually detecting large, but dark items, instead of small but bright items which was the original assumption. This lead to major implications for the calibration of optical and radar orbital debris detection systems.
  • It created a baseline event for researchers who wanted an idea of what a hypervelocity collision would be like in space.
  • Awareness was raised about the orbital debris problem.

Comet Discoveries

DesignationSolwind#Image dateDiscovery date
C/1979 Q1 (Solwind)1Aug 30th 1979Sep 1981
C/1981 B1 (Solwind)2Jan 27th 1981
C/1981 O1 (Solwind)3July 20th 1981
C/1981 V1 (Solwind)4Nov 4th 1981
C/1981 W1 (Solwind)7Nov 20th 1981June 30th 2005
C/1983 N2 (Solwind)8July 7th 1983July 19th 2005
C/1984 O2 (Solwind)6Sep 25th 1983
C/1984 O2 (Solwind)5July 28th 1984
C/1984 Q1 (Solwind)9Aug 23rd 1984July 22nd 2005
C/1984 R1 (Solwind)10Sep 17th 1984July 23rd 2005

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