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Atlas E/Trident
Part of Atlas
Atlas E + 1 x Trident upper stage.
AKA: Atlas/Trident E. Status: Retired 1968. First Launch: 1968-03-06. Last Launch: 1968-04-27. Number: 2 . Thrust: 1,731.00 kN (389,144 lbf). Gross mass: 130,000 kg (280,000 lb). Height: 25.00 m (82.00 ft). Diameter: 3.05 m (10.00 ft). Apogee: 1,500 km (900 mi).
More at: Atlas E/Trident.
Family:
orbital launch vehicle.
Country:
USA.
Launch Sites:
Vandenberg,
Vandenberg 576A3.
Stages:
Atlas E/F,
Atlas MA-3,
Trident Motor.
Agency:
Convair.
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 27 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A3.
LV Family:
Atlas.
Launch Vehicle:
Atlas E/Trident.
- RMP-B-7 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,600 km (900 mi).
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