Atlas E/Trident (original) (raw)

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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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