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ABRES
American Advanced Ballistic Re-Entry System Project, a military joint-service program for reentry vehicle research, development, and testing, established in 1963 and conducting many test launches over the following decades.
Subtopics
| AMaRV American Advanced Maneuverable Reentry Vehicle. An ABM-eluding prototype ICBM warhead built by McDonnell-Douglas and flown three times on Minuteman 1 test vehicles in 1979-1981. |
1963 March 1 - .
21:00 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC11.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES REX-I / Pod 1 Re-entry vehicle test - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1963 April 27 - .
02:03 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC11.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES REX-II re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1963 May 14 - .
- Advanced Ballistic Reentry System (ABRES) program established. - .
Related Persons: ABRES.
Spacecraft: ABRES.
The Advanced Ballistic Reentry System (ABRES) program, Program 627A, was established as a Defense Department joint-service program for reentry vehicle research, development, and testing. The Deputy for Ballistic Missile Reentry Systems (D/BMRS) office, established at Headquarters Ballistic Systems Division at Norton AFB in February 1963 would manage the program. The program director for ABRES would be Colonel Darwin C. Middlekauff, BSD's Deputy for Ballistic Missile Reentry Systems.
1963 October 28 - .
03:15 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC11.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
FAILURE: Failure.
Failed Stage: 1.
- ABRES WAC-1 / Pod 21 Reentry test / plume mission - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 500 km (310 mi).
1963 November 4 - .
09:34 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES REX-III re-entry vehicle test flight - .
Nation: USA.
Agency: USAF SAC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi). The first Advanced Ballistic Reentry System (ABRES) program launch from Vandenberg was successfully completed when SAC's Atlas D booster (232D) carried the Chrysler-built REX-3 reentry vehicle down the Pacific Missile Range. .
1963 December 18 - .
09:52 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES LORV-8 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF SAC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
Atlas 109F was the final Atlas research and development flight test missile to be launched. Since the first attempted launch of a Series A Atlas on 11 June 1957, 95 Atlas missiles had been used in the R&D program - eight As, nine Bs, six Cs, 32 Ds, 24 Es, and 16 Fs. All but 12 of these were launched from Cape Canaveral. Of the 95 launches, 57 were considered successful while 38 were failures.
1964 February 10 - .
Launch Site:
Green River.
Launch Complex:
Green River Pad 2.
LV Family:
Athena RTV.
Launch Vehicle:
Athena RTV.
FAILURE: Failure.
- USAF A001 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF.
Spacecraft: ABRES.
Apogee: 40 km (24 mi).
The first Athena test missile was launched from Green River, Utah, toward the White Sands Missile Range (WSMR) in New Mexico. The Athena research rocket was designed for the support of the Advanced Ballistic Reentry Systems (ABRES) program. Subscale models of ballistic reentry vehicles would be flown on the Athenas to test reentry vehicle concepts and phenomena. This first missile only had two operational stages, and several system failures resulted in the premature impact of the missile some 11 miles from Durango, Colorado. This was the first of several hundred launches from Green River, Utah, to impact points in the US Army's White Sands Missile Range in New Mexico. The Athena was designed to simulate the re-entry environment of an intercontinental ballistic missile and was one of the few examples of sustained interstate missile tests within the United States.
1964 February 25 - .
20:22 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC11.
LV Family:
Atlas.
Launch Vehicle:
Atlas E.
- ABRES WAC-3 / Pod 18 Re-entry vehicle test - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,600 km (900 mi). The first and only Atlas E (5E) ABRES vehicle to be launched from Cape Canaveral completed a successful flight down the Atlantic Missile Range..
1964 April 1 - .
20:22 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC11.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES WAC-2 / Pod 2 Reentry test / plume mission - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi). The last of four Atlas F (137F) ABRES test missiles was flown down the Atlantic Missile Range from Cape Canaveral. .
1964 June 18 - .
14:56 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES LORV-1 / Pod 31 Re-entry vehicle test - .
Nation: USA.
Agency: USAF SAC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1964 September 15 - .
15:27 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES LORV-3 / Pod 26 Re-entry vehicle test - .
Nation: USA.
Agency: USAF SAC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1964 December 1 - .
08:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES LORV-5 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF SAC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1965 February 27 - .
11:11 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES LORV-4 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF SAC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1965 March 12 - .
23:21 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576B3.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES MTV-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF SAC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1965 March 26 - .
09:01 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES LORV-7 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1965 April 6 - .
13:34 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576B1.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES WAC-4 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1965 June 8 - .
15:17 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES LORV-6 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1965 August 4 - .
12:43 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576B1.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES WAC-5 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1965 August 5 - .
13:21 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A2.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES LORV-2A re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi). The first Atlas F (147F) Advanced Ballistic Reentry Systems (ABRES) program launch was conducted at Vandenberg. The four previous Atlas F/ABRES launches were from Cape Canaveral, and the rest would be conducted on the Western Test Range. .
1966 May 13 - .
11:43 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576B1.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES WAC-5A re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1966 August 8 - .
17:47 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A2.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
FAILURE: Failure.
Failed Stage: 1.
- ABRES MBRV-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 500 km (310 mi).
1966 October 11 - .
19:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A2.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
FAILURE: Failure.
Failed Stage: 1.
- ABRES SBGRV-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 50 km (31 mi).
1967 January 18 - .
01:34 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A2.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES TVX-13 (21) re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1967 January 22 - .
15:44 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576B2.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES Mk 12R PDV re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1967 February 13 - .
22:05 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A3.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES TX-22 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1967 March 16 - .
17:56 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A2.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES MBRV-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi). The second Maneuvering Ballistic Reentry Vehicle (MBRV-2) was launched down the Western Test Range by Atlas 151F. Performance of the launch vehicle was satisfactory, but the MBRV failed to accomplish its planned reentry. .
1967 April 7 - .
11:19 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576B2.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES AX-1 / Pod 30 Reentry test / ionosphere mission - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1967 May 19 - .
22:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES SBGRV-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1967 June 9 - .
10:23 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A3.
LV Family:
Atlas.
Launch Vehicle:
Atlas F/Trident.
- ABRES SPDS (RMP-B-1) re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1967 July 1 - .
LV Family:
Minuteman.
- Space and Missile Systems Organization (SAMSO) created. - .
Spacecraft: ABRES.
The functions and personnel of Space Systems Division and Ballistic Systems Division were combined to form the new Space and Missile Systems Organization (SAMSO). Major General Paul T. Cooper, former SSD commander, becoming Deputy Commander for Space, and Major General John L. McCoy, the last BSD commander, becoming Deputy Commander for Missiles. Headquarters SAMSO took over SSD headquarters while General McCoy remained at Norton AFB with the Minuteman and Advanced Ballistic Reentry Systems (ABRES) program offices.
1967 July 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576B2.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES PDV re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1967 July 29 - .
08:48 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A2.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES MBRV-3 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
Launched from Vandenberg AFB atop Atlas booster 150F, the third Maneuvering Ballistic Reentry Vehicle (MBRV-3) achieved the first successful flight and reentry of a maneuvering ballistic reentry vehicle in the Advanced Ballistic Reentry Systems (ABRES) program. MBRV-3 successfully accomplished its planned terminal maneuver during reentry, and all objectives were achieved.
1967 October 11 - .
11:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576B3.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES TVX-13 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi).
1967 October 14 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A2.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES MBRV-4 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1967 November 7 - .
13:17 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576B2.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
- ABRES Mk 11 AX-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,800 km (1,100 mi). Atlas 94D was the 91st, and last, D series missile to be launched from Vandenberg AFB since 12D was launched on 9 September 1959. Final launch of an Atlas D missile (first operational at Vandenberg on 9 September 1959)..
1967 November 10 - .
12:20 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES BGRV-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1968 February 26 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES BGRV-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi). The Boost Glide Re-entry Vehicle was launched from Vandenberg AFB, California to the area of Wake Island in the Pacific Ocean. It was launched from an Atlas missile booster and served to provide data on hypersonic manoeuvring flight characteristics..
1968 March 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A3.
LV Family:
Atlas.
Launch Vehicle:
Atlas E/Trident.
- RMP-B-6 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,600 km (900 mi). The Air Force Western Test Range supported the initial west coast use of an Atlas E (74E) as a booster in an Advanced Ballistic Reentry Systems (ABRES) reentry vehicle development program. .
1968 April 18 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas E.
- ABRES RVTO-1A-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,600 km (900 mi).
1968 May 3 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A2.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
FAILURE: Failure.
Failed Stage: 1.
- ABRES Penaid TVX re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 100 km (60 mi).
1968 June 1 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A2.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES PDV re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1968 June 29 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES RVTO-1A-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1969 August 20 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES RVTO-1A-5 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1969 December 3 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES RVTO-1A-6 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1970 June 9 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES RVTO-1A-7 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1970 December 22 - .
08:38 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A3.
LV Family:
Atlas.
Launch Vehicle:
Atlas F/Trident.
- ABRES RVTO-2A-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1971 April 5 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES LAR-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1971 June 29 - .
13:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A3.
LV Family:
Atlas.
Launch Vehicle:
Atlas F/Trident.
- ABRES RVTO-2A-3 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1971 September 1 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- ABRES LAR-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
1972 March 17 - .
15:31 GMT - .
Launch Site:
Green River.
LV Family:
Athena RTV.
Launch Vehicle:
Athena H.
- SAMAST 1B re-entry vehicle test flight - .
Nation: USA.
Agency: USAF.
Spacecraft: ABRES.
Apogee: 281 km (174 mi).
The third Athena H rocket was launched from the Green River, Utah, launch complex. The flight test completed qualification of the vehicle for operational use in the Advanced Ballistic Reentry Vehicle (ABRES) program managed by SAMSO's Deputy for Reentry Systems (RS).
1972 June 30 - .
LV Family:
Minuteman.
- ABRES program office move. - .
Related Persons: ABRES.
Spacecraft: ABRES.
SAMSO1s Deputy for Reentry Systems (RS), the Advanced Ballistic Reentry Systems (ABRES) program office, completed its move from Norton AFB to Los Angeles Air Force Station..
1972 August 12 - .
09:25 GMT - .
Launch Site:
Green River.
LV Family:
Athena RTV.
Launch Vehicle:
Athena H.
- RVTO-3B-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF.
Spacecraft: ABRES.
Apogee: 200 km (120 mi). The first operational flight of an Athena H configuration booster was made from Green River, Utah, to the White Sands Missile Range carrying an Advanced Ballistic Reentry Systems (ABRES) payload. .
1973 March 9 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES NTV-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1973 August 24 - .
07:15 GMT - .
Launch Site:
Green River.
LV Family:
Athena RTV.
Launch Vehicle:
Athena H.
- ABC-3 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF.
Spacecraft: ABRES.
Apogee: 200 km (120 mi).
An Athena H missile was fired from the launch complex at Green River, Utah, carrying an Advanced Ballistic Reentry System (ABRES) payload. This was the 11th Athena H to be fired from Green River in support of the ABRES program and the 141st Athena to be launched from Green River since the beginning of the program in February 1964. Following this launch, the Green River complex was closed and Athena launch operations were transferred to Wake Island.
1973 September 30 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A1.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- BMRS ACE-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
Atlas 108F, carrying the Advanced Control Experiment 1 (ACE 1) vehicle, was launched from Vandenberg AFB and impacted in the Kwajalein area. The ACE 1 vehicle was to test the development of a preprototype of maneuvering reentry vehicle (MaRV) as part of the Advanced Ballistic Reentry Systems (ABRES) program.
1974 July 11 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF03.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES/SAMAST re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
First use of the Minuteman I booster, replacing the Atlas, for the ABRES program. The Sandia ABRES Materials and Systems Test 02/Miniature Instrumented Nosetip Test (SAMAST 02/MINT) reentry vehicles were successfully launched on a Minuteman I booster out of Vandenberg AFB. The Sandia ABRES Materials and Systems Test 02/Miniature Instrumented Nosetip Test (SAMAST 02/MINT) reentry vehicles were successfully launched on a Minuteman I booster out of Vandenberg AFB.
1974 October 14 - .
04:46 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A3.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- BMRS RVTO-3A-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,400 km (800 mi).
Surplus Atlas 31F was launched from Vanden-berg AFB carrying a Reentry Vehicles Technology and Observables (RVT0-3A-1) payload. This successful launch and flight marked the apparent end of the use of Atlas D,E, and F ICBMs in support of various Advanced Ballistic Reentry Systems (ABRES) and other governmental agency programs. Since Atlas 159D was launched from Vandenberg AFB on 26 October 1962 in support of the Nike Targets Program, a total of 113 Atlas missiles - 54Ds, 4Es, and 55Fs - have been launched with only 11 failures.
1975 May 23 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF03.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES NTV-3 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi). Nosetip Technology Vehicle-03 was successfully launched from Vandenberg Air Force Base, California..
1975 Nov - .
Launch Vehicle:
AICBM.
- AICBM cancelled. - .
Related Persons: ABRES.
The development program for a large, advanced ballistic reentry vehicle was cancelled..
1976 February 27 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF03.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
1976 March 9 - .
Launch Site:
Wallops Island.
LV Family:
Athena RTV.
Launch Vehicle:
Athena RTV.
- ABRES Re-entry Vehicle test - .
Nation: USA.
Agency: Sandia,
USAF.
Spacecraft: ABRES.
Apogee: 200 km (120 mi). The 37th launch of the Sandia ABRES Materials Study (SAMS) program occurred from Wallops into inclement weather. It tested the Aerojet platelet tip transpiration-cooled nosetip..
1976 March 27 - .
Launch Site:
Wallops Island.
LV Family:
Athena RTV.
Launch Vehicle:
Athena RTV.
- ABRES Re-entry Vehicle test - .
Nation: USA.
Agency: Sandia,
USAF.
Spacecraft: ABRES.
Apogee: 200 km (120 mi). 38th launch of the Sandia ABRES Materials Study (SAMS) program occurred from Wallops Flight Center, Virginia, into inclement weather. It tested the General Electric fine-weave carbon-carbon nosetip..
1976 April 25 - .
Launch Site:
Wallops Island.
LV Family:
Athena RTV.
Launch Vehicle:
Athena RTV.
- ABRES Re-entry Vehicle test - .
Nation: USA.
Agency: Sandia,
USAF.
Spacecraft: ABRES.
Apogee: 200 km (120 mi). The 39th and last launch of the Sandia ABRES Materials Study (SAMS) program occurred from Wallops Flight Center, Virginia into inclement weather. It tested the Aeronutronics scan tip..
1976 August 21 - .
03:40 GMT - .
Launch Site:
Kwajalein.
Launch Complex:
Kwajalein RN.
LV Family:
Hydac.
Launch Vehicle:
Nike Hydac.
FAILURE: Failure.
- TREP ABRES Density Aeronomy mission - .
Nation: USA.
Agency: USAF GL.
Spacecraft: ABRES.
Apogee: 15 km (9 mi).
1976 September 3 - .
- AMaRV contract award. - .
Spacecraft Bus: ABRES.
Spacecraft: AMaRV.
McDonnell Douglas Astronautics Company was awarded a $52.1 million contract for the development and flight test of two advanced maneuvering reentry vehicles (AMaRV)..
1976 September 9 - .
- The advanced maneuvering reentry vehicle (AMaRV) development program began. - .
Spacecraft Bus: ABRES.
Spacecraft: AMaRV.
1976 December 8 - .
- Advanced ballistic reentry vehicle contract. - .
Related Persons: ABRES.
SAMSO awarded Avco Corporation a 34-month, $26.7 million contract to design, build, and flight test an advanced ballistic reentry vehicle (ABRV)..
1976 December 15 - .
- AMaRV - .
Spacecraft Bus: ABRES.
Spacecraft: AMaRV.
The system design review of the advanced maneuvering reentry vehicle (AMaRV) was held successfully..
1977 Jan - .
- Advanced Ballistic Reentry Vehicle. - .
Related Persons: ABRES.
Spacecraft Bus: ABRV.
Avco Corporation began work on a system design for an Advanced Ballistic Reentry Vehicle..
1977 May 18 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES TDV-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
TDV-1, the first of three technology development vehicle flights in CY 1977, was successfully launched from Vandenberg AFB to the Kwajalein missile range on a Minuteman I booster. It successfully conducted complex experiments dealing with nosetip materials, aerodynamics, and electronics.
1977 May 18 - .
13:43 GMT - .
Launch Site:
Kwajalein.
Launch Complex:
Kwajalein RN.
LV Family:
Hydac.
Launch Vehicle:
Nike Hydac.
- ABRES Density / TDV-1 Aeronomy mission - .
Nation: USA.
Agency: USAF GL.
Spacecraft: ABRES.
Apogee: 188 km (116 mi).
1977 Aug - .
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- Dormant Inertial Navigation System - .
Spacecraft Bus: ABRES.
Spacecraft: AMaRV.
The Reentry Systems program office held a Preliminary Design Review of the design by Honeywell, Incorporated for the DINS (Dormant Inertial Navigation System)..
1977 Aug - .
- System Design Review for advanced ballistic reentry vehicles. - .
Related Persons: ABRES.
The Reentry Systems program office held a System Design Review of the Avco Corporation's design concept for advanced ballistic reentry vehicles employing Almendro and Muenster warheads..
1977 September 3 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES TDV-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
TDV-2, the second of three technology development vehicle flights in CY 1977, was successfully launched from Vandenberg AFB to the Kwajalein missile range on a Minuteman I booster. It successfully conducted complex experiments dealing with nosetip materials, aerodynamics, and electronics. A P 06-L star traffic decoy was successfully tested on the same flight.
1977 Oct - .
- Work on the inertial measurement unit for the AMaRV was completed. - .
Spacecraft Bus: ABRES.
Spacecraft: AMaRV.
Work on the SHIP inertial measurement unit for the AMaRV was completed by the Kearfott Division of the Singer Company. The guidance and navigation subsystem was to be flown on the first AMaRV..
1977 October 28 - .
- Terminal sensor for the AMaRV flight-tested for the first time. - .
Spacecraft Bus: ABRES.
Spacecraft: AMaRV.
The PDMM (Pulse Doppler-MAP Match) terminal sensor for the AMaRV was flight-tested for the first time on board a C-141 aircraft over Cape Cod. By the end of the year, it had completed five tests..
1977 Nov - .
- Design work began on an advanced nosetip for ABRES. - .
Related Persons: ABRES.
Spacecraft: ABRES.
Design work by Ford Aerospace and Communications Corporation began on an advanced graphite plug nosetip subsystem for ABRES small reentry vehicles..
1977 November 13 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES TDV-3 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1977 Dec - .
Launch Vehicle:
Peacekeeper.
- Reentry vehicles for use with Peacekeeper warhead. - .
Spacecraft: ABRES.
The Reentry Systems program office held a preliminary design review for the first two reentry vehicles designed by the Avco Corporation for use with the Almendro (Peacekeeper Mk 21 / W87) warhead..
1978 Jan - .
- AMaRV critical design review. - .
Spacecraft Bus: ABRES.
Spacecraft: AMaRV.
The Advanced Maneuvering Reentry Vehicle underwent a successful critical design review..
1978 April 5 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES TREP-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1978 May - .
- A successful critical design review was held for the Dormant Inertial Navigation System (DINS). - .
Spacecraft Bus: ABRES.
Spacecraft: AMaRV.
The DINS, which employed a laser gyro, was intended to function as the navigation subsystem in a manuevering reentry vehicle and was to be flight tested aboard the second Advanced Maneuvering Reentry Vehicle in 1979..
1978 June 16 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF03.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES ANT-3 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi). Four small reentry vehicles were successfully launched down the Western Test Range in an effort to evaluate the performance of several nosetip materials in clear weather. The launch was referred to as Advanced Nosetip Test III (A.N.T. III). .
1978 July 4 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES ANT-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi). Four small reentry vehicles were successfully launched down the Western Test Range in an effort to evaluate the performance of various nosetip materials in severe weather. The launch was referred to as Advanced Nosetip Test II (A.N.T. II). .
1978 November 27 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES ANT-3A re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1978 Dec - .
- ABRES Transpiration Cooled Nosetip cancelled - .
Related Persons: ABRES.
Spacecraft: ABRES.
SAMSO cancelled plans for flight-testing the Transpiration Cooled Nosetip (TCNT). The TCNT, which was an actively cooled reentry vehicle nosetip, had been under development as part of ABRES.Flight-test of the TCNT was cancelled due to funding and design problems that had plagued the development effort.
1979 Jan - .
LV Family:
Trident.
- Mark 500 Penetration Aid Concept Selection Study. - .
Related Persons: ABRES.
Spacecraft: ABRES.
The ABRES program office participated in a Mark 500 Penetration Aid Concept Selection Study involving the Aerospace Corporation, MIT Lincoln Laboratory, and other contractors. Participants in the study selected a penetration aid concept for the Navy's Trident C4/Mark 500 system.
1979 January 19 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES STREP-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
STREP-1, an ABRES flight test conducted in support of the Army's System Technology Reentry Experiments Program, was launched on a Minuteman I booster from Vandenberg AFB to Kwajalein missile range. The primary mission was successful, but a secondary payload, the advanced Star decoy sponsored by ABRES, deployed improperly because of improper loading, and data on its performance could not be collected.
1979 January 24 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF03.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES ABRV-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1979 Mar - .
- Tests of a position-fixing system for the AMaRV. - .
Spacecraft Bus: ABRES.
Spacecraft: AMaRV.
A C-141 aircraft completed data collection flights using the Pulse Doppler MAP Match (PDMM) system, a candidate position-fixing system for the AMaRV..
1979 Jun - .
- Position-fixing system for AMaRV. - .
Spacecraft Bus: ABRES.
Spacecraft: AMaRV.
A procurement contract with Goodyear Aerospace Corporation for the Range Only Correlation System (ROCS), a candidate position-fixing system for the AMaRV, was initiated..
1979 July 5 - .
- Advanced Maneuvering Reentry Vehicle (AMaRV) flight test scheduled for November 1979. - .
Spacecraft Bus: ABRES.
Spacecraft: AMaRV.
The final physical configuration audit of the Advanced Maneuvering Reentry Vehicle (AMaRV) flight test vehicle was completed preparatory to a flight test scheduled for November 1979..
1979 July 5 - .
- ABRES transferred. - .
Related Persons: ABRES.
Spacecraft: ABRES.
The Reentry Systems Program Office (ABRES) was transferred to the Deputy for ICBMs at Norton AFB, California..
1979 July 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF03.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
1979 August 3 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES STREP-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1979 Sep - .
- Dormant Inertial Navigation System (DINS) flight unit - .
Spacecraft Bus: ABRES.
Spacecraft: amarv.
The first Dormant Inertial Navigation System (DINS) flight unit, built by the Avionics Division of Honeywell, Inc. It was delivered to McDonnell Douglas Astronautics Company for installation xn the second scheduled AMaRV flight test vehicle. DINS was a laser-gyro-based strapdown inertial navigation system intended for use on maneuvering reentry vehicles.
1979 September 22 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES ABRV-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1979 September 25 - .
Launch Site:
Barking Sands.
LV Family:
Hydac.
Launch Vehicle:
Sergeant Hydac.
- HAVE LENT IV ABRES test - .
Nation: USA.
Agency: USAF.
Spacecraft: ABRES.
Apogee: 400 km (240 mi).
The first of two secondary rocket flight tests designated HAVE LENT IV successfully demonstrated the use of aerosol masking dispensers as a penetration aids. The vehicle was a Sergeant-Hydac rocket launched from Barking Sands, Hawaii. Data collection was limited because of erratic behavior of the rocket. The mission was sponsored by ABRES.
1979 December 20 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF03.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES AMARV-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1980 March 15 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES ABRV-3 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1980 April 10 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF03.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES STREP-4 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1980 September 15 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES STREP-3 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1980 October 8 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF03.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES AMARV-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1980 December 16 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES ABRV-4 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1981 February 18 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES IRS-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1981 March 15 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF03.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES TDV-4 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1981 April 4 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES Mk500-PAS-1 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1981 September 12 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES Mk500-PAS-2 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
1981 October 4 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF03.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- ABRES AMARV-3 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Spacecraft: ABRES.
Apogee: 1,300 km (800 mi).
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