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ATS-2
Part of ATS
ATS-2 Credit: NASA |
American communications technology satellite. ATS 2. ATS-2 was placed into an undesirable orbit due to a launch vehicle failure.
AKA: Applications Technology Satellite. Status: Operational 1967. First Launch: 1967-04-06. Last Launch: 1967-04-06. Number: 1 . Gross mass: 370 kg (810 lb). Height: 1.80 m (5.90 ft).
Atmospheric torques in this orbit overcame the satellite's gravity gradient stabilization system, and caused a slow tumble. Although the satellite remained functional, the satellite was deactivated after six months due to the limited amount of data that could be received from the spacecraft. Spacecraft: Aluminum structure, drum solar array providing 125W BOL, 2 6 Ah NiCd batteries, gravity gradient stabilization. Payload: Meteorological experiments, C-band communications package
Family:
Communications technology sat,
Geosynchronous orbit,
Technology.
Country:
USA.
Launch Vehicles:
Atlas,
Atlas SLV-3 Agena D.
Projects:
ATS.
Launch Sites:
Cape Canaveral,
Cape Canaveral LC12.
Agency:
NASA,
NSF,
Hughes.
Bibliography:
2,
278,
279,
3570,
3571,
3574,
3575,
3576,
3577,
3578,
3579,
3580,
6.
Photo Gallery
| ATS 2 Credit: Manufacturer Image |
1967 April 6 - .
03:23 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC12.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
FAILURE: Partial Failure..
Failed Stage: U.
- ATS 2 - .
Payload: ATS A. Mass: 370 kg (810 lb). Nation: USA.
Agency: NASA Greenbelt.
Program: ATS.
Class: Technology.
Type: Communications technology satellite. Spacecraft Bus: ATS.
Spacecraft: ATS-2.
Decay Date: 1969-09-02 . USAF Sat Cat: 2743 . COSPAR: 1967-031A. Apogee: 11,119 km (6,909 mi). Perigee: 177 km (109 mi). Inclination: 28.40 deg. Period: 218.80 min. Launch vehicle failure left in useless orbit; communications tests..
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