Scout E-1

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Scout E-1

Part of Scout

Scout
Credit: NASA

American all-solid orbital launch vehicle. Five stage vehicle consisting of 1 x Algol 3A + 1 x Castor 2 + 1 x Antares 2 + 1 x FW4S + 1 x BE-3

Status: Retired 1974. First Launch: 1974-06-03. Last Launch: 1974-06-03. Number: 1 . Payload: 200 kg (440 lb). Thrust: 464.00 kN (104,311 lbf). Gross mass: 20,600 kg (45,400 lb). Height: 25.00 m (82.00 ft). Diameter: 1.14 m (3.74 ft). Apogee: 130,000 km (80,000 mi).

LEO Payload: 200 kg (440 lb).

More at: Scout E-1.

Family: all-solid, orbital launch vehicle. Country: USA. Spacecraft: Hawkeye. Projects: Explorer. Launch Sites: Vandenberg, Vandenberg SLC5. Stages: Antares 2, Altair 3, Algol 3A, BE-3, Castor 2. Agency: Vought.

1974 June 3 - . 23:09 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout E-1.

Explorer 52 - . Payload: Hawkeye. Mass: 27 kg (59 lb). Nation: USA. Agency: NASA Langley. Program: Explorer. Class: Astronomy. Type: Solar satellite. Spacecraft: Hawkeye. Decay Date: 1978-04-30 . USAF Sat Cat: 7325 . COSPAR: 1974-040A. Apogee: 125,569 km (78,024 mi). Perigee: 469 km (291 mi). Inclination: 89.00 deg. Period: 3,032.00 min. Solar wind experiments. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .

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