Delta 3913 (original) (raw)

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Delta 3913

Part of Thor

American orbital launch vehicle. Four stage vehicle consisting of 9 x Castor 4 + 1 x ELT Thor/RS-27 + 1 x Delta P /TR-201 + 1 x Star 37N

Status: Retired 1981. First Launch: 1981-08-03. Last Launch: 1981-08-03. Number: 1 . Thrust: 3,188.00 kN (716,690 lbf). Gross mass: 190,000 kg (410,000 lb). Height: 35.00 m (114.00 ft). Diameter: 2.44 m (8.00 ft). Apogee: 25,000 km (15,000 mi).

More at: Delta 3913.

Family: orbital launch vehicle. Country: USA. Spacecraft: Dynamics Explorer. Launch Sites: Vandenberg, Vandenberg SLC2W. Stages: Delta P, Delta Thor RS27, Castor 4, Star 37N. Agency: Douglas.

1981 August 3 - . 09:56 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Thor. Launch Vehicle: Delta 3913. FAILURE: Partial Failure.. Failed Stage: U.

Dynamics Explorer 1 - . Payload: DE A. Mass: 403 kg (888 lb). Nation: USA. Agency: NASA Greenbelt. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Dynamics Explorer. USAF Sat Cat: 12624 . COSPAR: 1981-070A. Apogee: 23,232 km (14,435 mi). Perigee: 528 km (328 mi). Inclination: 88.60 deg. Period: 409.20 min. Dynamics Explorer 1..
Dynamics Explorer 2 - . Payload: DE B. Mass: 403 kg (888 lb). Nation: USA. Agency: NASA Greenbelt. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Dynamics Explorer. Decay Date: 1983-02-19 . USAF Sat Cat: 12625 . COSPAR: 1981-070B. Apogee: 1,002 km (622 mi). Perigee: 304 km (188 mi). Inclination: 90.00 deg. Period: 97.80 min. Dynamics Explorer 2..

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