Encyclopedia Astronautica
Atlas/Trident F


Atlas F + 1 x Trident upper stage.

Failures: 3. First Fail Date: 1967-10-27. Last Fail Date: 1969-10-10.

Gross mass: 130,000 kg (280,000 lb).
Height: 25.00 m (82.00 ft).
Diameter: 3.05 m (10.00 ft).
Thrust: 1,731.00 kN (389,144 lbf).
Apogee: 1,500 km (900 mi).
First Launch: 1967.06.09.
Last Launch: 1971.06.29.
Number: 17 .

More... - Chronology...


Associated Countries
See also
  • Atlas The Atlas rocket, originally developed as America's first ICBM, was the basis for most early American space exploration and was that country's most successful medium-lift commercial launch vehicle. It launched America's first astronaut into orbit; the first generations of spy satellites; the first lunar orbiters and landers; the first probes to Venus, Mars, Mercury, Jupiter, and Saturn; and was America's most successful commercial launcher of communications satellites. Its innovative stage-and-a-half and 'balloon tank' design provided the best dry-mass fraction of any launch vehicle ever built. It was retired in 2004 after 576 launches in a 47-year career. More...

Associated Manufacturers and Agencies
  • Convair American manufacturer of rockets, spacecraft, and rocket engines. Convair, USA. More...

Associated Launch Sites
  • Vandenberg Vandenberg Air Force Base is located on the Central Coast of California about 240 km northwest of Los Angeles. It is used for launches of unmanned government and commercial satellites into polar orbit and intercontinental ballistic missile test launches toward the Kwajalein Atoll. More...
  • Vandenberg 576A3 Atlas, AMROC launch complex. Originally an Atlas 576 SMS ICBM pad. Upgraded for use as ABRES pad in 1965, and for BMRS program in 1971. More...

Associated Stages
  • Atlas MA-3 Lox/Kerosene propellant rocket stage. Loaded/empty mass 3,174/3,174 kg. Thrust 1,644.96 kN. Vacuum specific impulse 290 seconds. More...
  • Atlas E/F Lox/Kerosene propellant rocket stage. Loaded/empty mass 117,826/4,926 kg. Thrust 386.30 kN. Vacuum specific impulse 316 seconds. More...

Atlas/Trident F Chronology


1967 June 9 - . 10:23 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 122F.
  • ABRES SPDS (RMP-B-1) re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1967 July 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 114F.
  • RMP-B-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1967 October 27 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 81F. FAILURE: Failure. Failed Stage: 1.
  • RMP-B-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1.00 km (0.60 mi).

1967 December 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 117F.
  • RMP-B-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1968 January 31 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 94F.
  • RMP-B-5 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1968 June 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 86F.
  • RMP-B-8 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1968 September 25 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 99F.
  • RMP-B-9 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1968 November 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 56F. FAILURE: Failure. Failed Stage: 1.
  • RMP-B-10 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 10 km (6 mi).

1969 January 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 70F.
  • RMP-B-11 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1969 September 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 100F.
  • RMP-B-12 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1969 October 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 98F. FAILURE: Failure. Failed Stage: 1.
  • RMP-B-13 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 10 km (6 mi).

1969 December 12 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 93F.
  • RMP-B-14 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1970 February 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 96F.
  • RMP-B-15 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1970 March 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 28F.
  • RMP-B-16 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1970 May 30 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 91F.
  • RMP-B-17 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. 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/Trident F. LV Configuration: Atlas F/Trident 105F.
  • ABRES RVTO-2A-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. 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/Trident F. LV Configuration: Atlas F/Trident 103F.
  • ABRES RVTO-2A-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

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