ASM-135 ASAT

Infobox Weapon
is_missile=yes
name=ASM-135 ASAT


caption=
origin=
type=Anti-Satellite Missile
used_by=
manufacturer=LTV Aerospace
unit_cost=
production_date=1984
service=Not Deployed (008)
engine=
weight=2600 lb (1,180 kg)
length=18 ft (5.48 m)
diameter=20 in (50.8 cm)
wingspan=
speed=>15,000 mph (24,000 km/h)
vehicle_range=403 miles (648 km)
ceiling=350 miles (563 km)
altitude=
filling=Kinetic Energy Kill
guidance=Infrared Homing Seeker
detonation=
launch_platform=F-15 Eagle

The ASM-135 ASAT is an air-launched anti-satellite multi stage missile that was developed by Ling-Temco-Vought (LTV) Aerospace. The ASM-135 was carried exclusively by the United States Air Force (USAF)'s F-15 Eagle fighter aircraft.

Development

Starting in the late 1950s, the United States began development of anti-satellite weapons. The first United States anti-satellite weapon was Bold Orion Weapon System 119B. Like the ASM-135, the Bold Orion missile was air launched; but in this case from a B-47 Stratojet. The Bold Orion was tested in 19 October 1959 against the Explorer 6 satellite. Edited By Bhupendra Jasani, "Space Weapons and International Security", A SIPRI Publication, Oxford University Press, 1987.] The two-stage Bold Orion missile passed within 4 miles (6.4 km) of Explorer 6. From this distance, only a nuclear warhead would have destroyed the target.Encyclopedia Astronautica, "Bold Orion", [http://www.astronautix.com/lvs/bolorion.htm] , web page retrieved on 3 November 2007.]

Starting in 1960 the Department of Defense (DoD) started a program called SPIN (SPace INtercept). In 1962, the United States Navy air launched rockets from an F-4D fighter as part of Project Hi-Hoe with the objective of developing an anti-satellite weapon.Federation of American Scientists Web Site, "FAS Space Policy Project - Military Space Programs", [http://www.fas.org/spp/military/program/asat/overview.htm] , web page retrieved on 3 November 2007.] Aerospace Web.org Website. "NOTSNIK, Project Pilot & Project Caleb" [http://www.aerospaceweb.org/question/spacecraft/q0271.shtml] retrieved on 5 November 2007.]

The United States developed direct ascent anti-satellite weapons. A United States Army Nike Zeus missile armed with nuclear warhead destroyed an orbiting satellite in May 1963. Paul B. Stares, "The Militarization of Space: U.S. Policy, 1945–1948", Cornell University Press, 1985.] One missile from this system known as Project MUDFLAP and later as Project 505 was available for launch from 1964 until 1967. A nuclear armed Thor anti-satellite system deployed by the United States Air Force under Program 437 eventually replaced the Project 505 Nike Zeus in 1967. The Program 437 Thor missile system remained in limited deployment until 1975. Peter L. Hays, "Struggling Towards Space Doctrine: U.S. Military Plans, Programs, and Perspectives during the Cold War," Ph.D. dissertation, Fletcher School of Law and Diplomacy, Tufts University, May 1994] . One drawback of nuclear armed anti-satellite weapons was they could also potentially damage United States reconnaissance satellites. As a result the United States anti-satellite weapons development effort were re-directed to develop systems that did not require the use of nuclear weapons.

After the Soviet Union demonstrated an operational co-orbital anti-satellite system, in 1978, U.S. President Jimmy Carter directed the USAF to develop and deploy a new anti-satellite system.Dr. Raymond L. Puffer, "The Death of a Satellite", [http://web.archive.org/web/20031218130538/www.edwards.af.mil/moments/docs_html/85-09-13.html] , Retrieved on November 3, 2007.]

In 1978, the USAF started a new program initially designated the Prototype Miniature Air-Launched Segment (PMALS) and Air Force System Command's Space Division established a system program office. The USAF issued a Request for Proposal for the Air Launched Miniature Vehicle. The requirement was for an air-launched missile that could be used against satellites in low earth orbit.

Design

In 1979, the USAF issued a contract to LTV Aerospace to begin work on the ALMV. The LTV Aerospace design featured a multi-stage missile with a infrared homing kinetic energy warhead. Directory of U.S. Military Rockets and Missiles. "Vought ASM-135 ASAT" [http://www.designation-systems.net/dusrm/m-135.html] Accessed on 2 November 2007.]

The ASM-135 was launched from an F-15A in a supersonic zoom climb. The F-15's mission computer and heads-up display were modified to provide steering directions for the pilot.

A modified Boeing AGM-69 SRAM missile with a Lockheed Propulsion Company LPC-415 solid propellant two pulse rocket engine was used as the first stage of the ASM-135 ASAT. Vought Heritage Website "ASAT Overview" [http://www.vought.com/heritage/products/html/asat.html] , retrieved on 3 November, 2007.]

The LTV Aerospace Altair 3 was used as the second stage of the ASM-135.Encyclopedia Astronautica. "Altair 3". [http://www.astronautix.com/stages/altair3.htm] . retrieved on 2 November 2007.] The Altair 3 used the Thiokol FW-4S solid propellant rocket engine. The Altair 3 stage was also used as the fourth stage for the Scout rocket and had been previously used in both the Bold Orion and HiHo anti-satellite weapons efforts. The Altair was equipped with Hydrazine fueled thrusters that could be used to point the missile towards the target satellite.

LTV Aerospace also provided the third stage for the ASM-135 ASAT. This stage was called Miniature Homing Vehicle (MHV) intercepter. Prior to being deployed the second stage was used to spin the MHV up to approximately 30 revolutions per second and point the MHV towards the target. Gregory Karambelas, edited by Sven Grahn, "The F-15 ASAT Story", [http://www.svengrahn.pp.se/histind/ASAT/F15ASAT.html] ]

A Honeywell ring laser gyroscope was used for spin rate determination and to obtain an inertial timing reference before the MHV separated from the second stage. The infrared sensor was developed by Hughes Research Laboratories. The sensor utilized a strip detector where four strips of Indium Bismuth were arranged in a cross and four strips were arranged as logarithmic spirals. As the detector was spun, the infrared target's position could be measured and as it crossed the strips in the sensors field of view. The MHV infrared detector was cooled by liquid helium from a dewar installed in place of the F-15's gun ammunition drum and from a smaller dewar located in the second stage of the ASM-135. Cryogenic lines from the second stage were retracted prior to the spin up of the MHV.

The MHV guidance system solely tracked targets in the field of view of the infrared sensor, but did not determine altitude, attitude, or range to the target. Direct Proportional Line of Sight guidance used information from the detector to maneuver and null out any line-of-sight change. A Bang-bang control system was used to fire 56 full charge "divert" and lower thrust 8 half charge "end-game" solid rocket motors arranged around the circumference of the MHV. The half charge 8 "end-game" motors were used to perform finer trajectory adjustments just prior to intercepting the target satellite. Four pods at the rear of the MHV contained small attitude control rocket motors. These motors were used to dampen off center rotation by the MHV.

Test launches

On 21 December 1982, an F-15A was used to perform the first captive carry ASM-135 test flight from the Air Force Flight Test Center, Edwards AFB, California in the United States.

On 20 August 1985 President Reagan authorized a test against a satellite. The test was delayed to provide notice to the United States Congress. The target was the Solwind P78-1, an orbiting solar observatory that was launched on 24 February 1979.

On 13 September 1985, Maj. Wilbert D. "Doug" Pearson, flying the "Celestial Eagle" F-15A 76-0084 launched an ASM-135 ASAT about 200 miles (322 km) west of Vandenberg Air Force Base and destroyed the Solwind P78-1 satellite flying at an altitude of 345 miles (555 km). Prior to the launch the F-15 flying at Mach 1.22 executed a 3.8g zoom climb at an angle of 65 degrees. The ASM-134 ASAT was automatically launched at 38,100 ft while the F-15 was flying at Mach .934. The 30 lb (13.6 kg) pound MHV collided with the 2,000 lb (907 kg) pound Solwind P78-1 satellite at closing velocity of 15,000 mph (24,140 km/h). Vought Heritage Website, [http://www.vought.com/heritage/products/html/asat.html] , Retrieved on November 4, 2007]

NASA learned of U.S. Air Force plans for the Solwind ASAT test in July 1985. NASA modeled the effects of the test. This model determined that debris produced would still be in orbit in the 1990s. It would force NASA to enhance debris shielding for its planned space station. NASA TP-1999-208856 David S.F. Portree and Joseph P. Loftus Jr. "Orbital Debries: A Chronology" ]

Earlier the U.S. Air Force and NASA had worked together to develop a Scout-launched target vehicle for ASAT experiments. NASA advised the U.S. Air Force on how to conduct the ASAT test to avoid producing long-lived debris. However, congressional restrictions on ASAT tests intervened.

In order to complete an ASAT test before an expected Congressional ban took effect (as it did in October 1985), the DoD determined to use the existing Solwind astrophysics satellite as a target.

NASA worked with the DoD to monitor the effects of the tests using two orbital debris telescopes and a reentry radar deployed to Alaska.

NASA assumed the torn metal would be bright. Surprisingly, the Solwind pieces turned out to appear so dark as to be almost undetectable. Only two pieces were seen. NASA Scientists theorized that the unexpected Solwind darkening was due to carbonization of organic compounds in the target satellite; that is, when the kinetic energy of the projectile became heat energy on impact, the plastics inside Solwind vaporized and condensed on the metal pieces as soot.

NASA utilized U.S. Air Force infrared telescopes to show that the pieces were warm with heat absorbed from the Sun. This added weight to the contention that they were dark with soot and not reflective. The pieces decayed quickly from orbit, implying a large area-to-mass ratio.

The Solwind test had three important results:

* It raised the possibility that the objects optical systems were detecting were large and dark, not small and bright as was generally assumed. This had implications for the calibration of optical and radar orbital debris detection systems.
* The test also created a baseline event for researchers seeking a characteristic signature of a hypervelocity collision in space.
* Awareness was raised about the orbital debris problem.

In the end, the Solwind ASAT test had few consequences for the planned U.S. space station as station completion was pushed beyond the mid-1990s. The record-high level of solar activity during the 1989-1991 solar maximum heated and expanded the atmosphere more than anticipated in 1985, accelerating Solwind debris decay.

15 ASM-135 ASAT missiles were produced and 5 missiles were flight tested

Operational History

The United States Air Force intended to modify 20 F-15A fighters from the 318th Fighter Intercepter Squadron based at McChord Air Force Base in the United States state of Washington and the 48th Fighter Interceptor Squadron based at Langley Air Force Base in the United States state of Virginia for the anti-satellite mission. Both squadrons had airframes modified to support the ASM-135 by the time the project was cancelled in 1988.McChord Air Museum Web Site. "McDonnell-Douglas F-15A Eagle". [http://www.mcchordairmuseum.org/REV%20B%20MAM%20COLLECTION%20F-15%20%20BORDER.htm] . Web page accessed 2 November 2007.]

The USAF had planned to deploy an operational force of 112 ASM-135 missiles.

The deployment of the ASM-135 was central to a policy debate in the United States over the strategic need for an anti-satellite weapon and the potential for anti-satellite weapon arms control with the Soviet Union. Starting in 1983, the United States Congress starting placing various restrictions on the ASM-135 program. In December 1985, included a ban on testing the ASM-135 on a target in space. This decision was made only a day after the Air Force sent two target satellites into orbit for its next round of tests. The Air Force continued to test the ASAT system in 1986, but stayed within the limits of the ban by not engaging a space-borne target.Union of Concerned Scientists Web Site. "A History of ASAT Programs". [http://www.ucsusa.org/global_security/space_weapons/a-history-of-asat-programs.html] . retrieved on 4 November 2007.]

In the same year the deployment of the ASM-135 was estimated to cost $5.3 billion dollars (US) up from the original $500 million dollar (US) estimate. The USAF scaled back the ASM-135 program by two-thirds in attempt to control costs. The USAF also never strongly supported the program and proposed canceling the program in 1987. In 1988, the Reagan Administration canceled the ASM-135 program because of technical problems, testing delays, and significant cost growth.

Variants

*ASM-135 - 15 missiles produced.
*CASM-135 - Captive carry version of ASM-135A with warhead simulator and inert motors.

Operator

*
** United States Air Force

urvivors

* CASM-135 currently on display at the Steven F. Udvar-Hazy Center, part of the Smithsonian National Air and Space Museum (NASM)'s annex at Washington Dulles International Airport in Chantilly, Virginia, United States.
* CASM-135 currently in storage at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Dayton, Ohio, United States.

Popular Culture

* The ASM-135 features prominently in the Tom Clancy novel "Red Storm Rising". Several USSR RORSATs are knocked out by F-15 launched ASATs.
* Capt. Todd Pearson son of Major General Wilbert D. "Doug" Pearson (ret.) flew the exact same F-15 Eagle (Celestial Eagle 76-0084), now assigned to the Florida Air National Guard 125th Fighter Wing on 13 September 2007. 22 years earlier the same aircraft had been used by Major General Pearson to accomplish the only successful satellite kill by an aircraft launched missile in history.
* The ASM-135 is featured on a 1:72 scale die-cast aircraft model from Dragon Models Limited. Dragon Models Limited Corporate Website. [http://www.dragon-models.com/html/50246p1.htm] Accessed on 2 November 2007.]

References

ee also

aircontent
comparable aircraft header=Comparable missiles
similar aircraft=
* MIG-31D Miniature ASAT (Russia)
* Project Bold Orion (USA)
* Project Hi-Hoe (USA)
* Project NOTSNIK (USA)
* Project Spike (USA)
* Project SRAM/LEAP (USA)
sequence=

* AIM-132 ASRAAM - UGM-133 Trident - MGM-134 Midgetman - ASM-135 - AGM-136 Tacit Rainbow - AGM-137 TSSAM - CEM-138 Pave Cricket
see also=
lists=
* List of military aircraft of the United States
* List of missiles

External links

* [http://www.svengrahn.pp.se/histind/ASAT/F15ASAT.html The F-15 ASAT story]