Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Atlas E/OIS
Status: Retired 1985. First Launch: 1985-03-13. Last Launch: 1985-03-13. Number: 1 . Thrust: 1,731.00 kN (389,144 lbf). Gross mass: 120,000 kg (260,000 lb). Height: 28.70 m (94.10 ft). Diameter: 3.05 m (10.00 ft). Apogee: 800 km (490 mi).
More at: Atlas E/OIS.
Family: orbital launch vehicle. Country: USA. Spacecraft: Geosat. Launch Sites: Vandenberg, Vandenberg SLC3W. Stages: Atlas E/F, Atlas MA-3, Star 27. Agency: Convair.
1985 March 13 - . 02:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3W. LV Family: Atlas. Launch Vehicle: Atlas E/OIS.
- Geosat - . Mass: 635 kg (1,399 lb). Nation: USA. Agency: USN. Class: Earth. Type: Civilian Radarsat. Spacecraft: Geosat. USAF Sat Cat: 15595 . COSPAR: 1985-021A. Apogee: 779 km (484 mi). Perigee: 775 km (481 mi). Inclination: 108.10 deg. Period: 100.40 min. Ocean sea height mapping. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C)..
Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use