Atlas IIIA
In-activeLockheed Martin (LMT)
May 24, 2000
Description
American orbital launch vehicle used between 2000 and 2005.
Specifications
-
Stages
2 -
Length
52.8 m -
Diameter
3.05 m -
Fairing Diameter
― -
Launch Mass
214.0 T -
Thrust
4149.0 kN
Family
-
Name
Atlas IIIA -
Family
― -
Variant
IIIA -
Alias
― -
Full Name
Atlas IIIA
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
8640.0 kg -
Geostationary Transfer
Orbit
4055.0 kg -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
Lockheed Martin
Commercial
None
LMT 1953Lockheed Martin's Space Division started in the production of missiles and later ICBM's in the 1950s. Their TITAN missile system was used for 12 Gemini spacecraft and the Voyager probes. They have worked largely in collaboration with NASA on many of their probes, landers, and spacecraft, and hope to play a key role in NASA's return to the moon in 2024.
Atlas Agena B | MBSAT
Lockheed Martin | United States of AmericaCape Canaveral SFS, FL, USA
March 13, 2004, 5:40 a.m.
Atlas Agena B | Eutelsat W4
Lockheed Martin | United States of AmericaCape Canaveral SFS, FL, USA
May 24, 2000, 11:10 p.m.
Status: Launch Successful
Mission:
The W satellites are designed to provide telecommunications services primarily over Europe (W1, W2, W3, W3A and W5) and communication services over Russia and Africa (W4). Eutelsat W4 is designed to provide 31 transponders at saturation. The W satellites have a minimum operational lifetime of 12 years. The spacecraft is based on the Spacebus-3000B2 platform.
Geostationary OrbitLong March 3B/E
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