Atlas III
From Wikipedia, the free encyclopedia
The maiden flight of the Atlas III |
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Fact sheet | ||
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Function | Medium expendable Launch vehicle | |
Manufacturer | Lockheed Martin | |
Country of origin | USA | |
Size | ||
Height | 52.8 m (173.2 ft) | |
Diameter | 3.05 m (10 ft) | |
Mass | 214,338 kg (472,338 lb) | |
Stages | 2 | |
Capacity | ||
Payload to LEO | Atlas IIIA: 8,640 kg (19,040 lb) Atlas IIIB: 10,218 kg (23,630 lb) |
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Payload to GTO |
Atlas IIIA: 4,055 kg (8,939 lb) Atlas IIIB: 4,500 kg (9,900 lb) |
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Launch History | ||
Status | Retired | |
Launch Sites | LC-36B, CCAFS | |
Total launches | 6 2 Atlas IIIA 4 Atlas IIIB |
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Successes | 6 | |
Maiden flight | Atlas IIIA: 24 May 2000 Atlas IIIB: 21 February 2002 |
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Last flight | Atlas IIIA: 13 March 2004 Atlas IIIB: 3 February 2005 |
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First Stage | ||
Engines | 1 RD-180 | |
Thrust | 4,148.7 kN (932,670 lbf) | |
Specific Impulse | 311 sec | |
Burn time | 132 seconds | |
Fuel | RP-1/LOX | |
Second Stage (Atlas IIIA) - Centaur (SEC) | ||
Engines | 1 RL-10A | |
Thrust | 99.2 kN (22,290 lbf) | |
Specific Impulse | 451 sec | |
Burn time | 738 seconds | |
Fuel | LH2/LOX | |
Second Stage (Atlas IIIB) - Centaur (DEC) | ||
Engines | 2 RL-10A | |
Thrust | 147 kN (22,290 lbf) | |
Specific Impulse | 449 sec | |
Burn time | 392 seconds | |
Fuel | LH2/LOX | |
The Lockheed Martin Atlas III was an American orbital launch vehicle, used between 2000 and 2005. It was the first member of the Atlas family to feature a "normal" staging method, compared to the previous Atlas variants, which were equipped with jettisonable engines on the first (sustainer) stage.
It consisted of two stages. The first stage was new, but the upper stage was the Centaur, which has been used on most American launch vehicles since the 1960s, and is still in use today on the Atlas V and Delta EELVs.
The first stage engines were Russian RD-180s, which are also used by the Atlas V. They are license-produced in the US by Pratt and Whitney.
The maiden flight of the Atlas III occurred on May 24, 2000, launching the Eutelsat W4 communications satellite into a geosynchronous orbit.
The Atlas III was produced in two versions. The baseline was the Atlas IIIA, but the Atlas IIIB, which featured a twin-engine version of the Centaur upper stage was also produced.
All Atlas III launches were made from Launch Complex 36B at Cape Canaveral Air Force Station.
The Atlas III made its last flight on February 3, 2005, with a classified payload for the United States National Reconnaissance Office.
Current: |
Ariane 5 • Atlas V • Cosmos-3M • Delta II • Delta IV • Dnipro • Geosynchronous Satellite Launch Vehicle • H-IIA • Long March • Minotaur • Pegasus • Polar Satellite Launch Vehicle • Proton • Rockot • Soyuz • Taurus • Tsyklon • Zenit |
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Planned: | |
Historical: |
Ariane 1 • Ariane 2/3 • Ariane 4 • Atlas ICBM • Atlas II • Atlas III • Black Arrow • Delta III • Diamant • Energia • Europa • M-V • N1 • R-7 Semyorka • Saturn I • Saturn IB • Saturn V • Saturn INT-21 • PGM-17 Thor • Titan (I, II, III, IV) • Voskhod • Vostok |