CONVAIR

Atlas SLV-3C Centaur

17FLIGHTS

88.2%SUCCESS

2FAILURES

6STREAK

Sep 1967FIRST FLIGHT

NOREUSABLE

HEIGHT21 m

DIAMETER3.05 m

LAUNCH MASS120 kg

STAGES2

ABOUT ATLAS SLV-3C CENTAUR

The Atlas-Centaur was a US expendable launch vehicle derived from the SM-65 Atlas D missile. Launches were conducted from Launch Complex 36 at the Cape Canaveral Air Force Station in Florida.

PAYLOAD CAPACITY

800 kg

TO LEO

1,764 lbs

DIMENSIONS

↕Height21 m (69 ft)

↔Diameter3.05 m (10 ft)

⚖Launch Mass120 kg (265 lbs)

▣Stages2

🔗 WIKIPEDIA

SATELLITES DEPLOYED (1)

Intelsat Epic14 launchesGEO

FLIGHT HISTORY

Atlas SLV-3C Centaur | Copernicus

Aug 21, 1972SUCCESS

Atlas SLV-3C Centaur | INTELSAT IV F5

Jun 13, 1972SUCCESS

Atlas SLV-3C Centaur | Pioneer 10

Mar 3, 1972SUCCESS

Atlas SLV-3C Centaur | INTELSAT IV F4

Jan 23, 1972SUCCESS

Atlas SLV-3C Centaur | INTELSAT IV F3

Dec 20, 1971SUCCESS

Atlas SLV-3C Centaur | Mariner 9

May 30, 1971SUCCESS

Atlas SLV-3C Centaur | Mariner 8

May 9, 1971FAILURE

Atlas SLV-3C Centaur | INTELSAT IV F2

Jan 26, 1971SUCCESS

⚙ RELATED ENGINES

BE-4Engine RD-180Engine RL-10Engine

🚀 OTHER CONVAIR VEHICLES

Atlas Agena A3 flights Atlas Agena D15 flights Atlas B1 flights Atlas Burner 22 flights Atlas Centaur4 flights Atlas Centaur D7 flights