Titan family

Titan 401A Centaur

RetiredUnited StatesLockheed MartinSpec: 401A Centaur

Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005.

Flights flown9
Success rate88.9%8/9
Payload to LEO21,680kg
Maiden flight1994-02-07
Peak year19943 flights

Titan 401A Centaur is built by Lockheed Martin of the United States. It first flew on 7 February 1994 and last flew on 12 August 1998.

Flight record

9 records
88.9% success rate8 of 9 flown · 1 failed
1994peak 1994 · 3 flights1998
First flight1994-02-07
Latest flight1998-08-12
Failures1
Consecutive successes0
Fastest turnaround56d 22h

Payload

Per mission profile
Low Earth orbit21,680kg
Geostationary transfer orbit9,000kg

Vehicle

401A Centaur spec
Stages3
Length63.1m
Diameter3.05m
Launch mass868t
Liftoff thrust14,200kN
Maiden flight1994-02-07
ReusableNo

Pads used

2 pads

Orbits delivered

2 orbits
Geostationary Orbit7Elliptical Orbit2

Launch history

9 launches
DateMissionPadOrbitOutcome
1998-08-12Titan 401A Centaur | Mercury 16Space Launch Complex 41Geostationary OrbitFailure
1997-11-08Titan 401A Centaur | NROL-4Space Launch Complex 41Geostationary OrbitSuccess
1996-04-24Titan 401A Centaur | Mercury 15Space Launch Complex 41Geostationary OrbitSuccess
1995-11-06Titan 401A Centaur | Milstar 2Space Launch Complex 40Geostationary OrbitSuccess
1995-07-10Titan 401A Centaur | Trumpet 2Space Launch Complex 41Elliptical OrbitSuccess
1995-05-14Titan 401A Centaur | Orion 3Space Launch Complex 40Geostationary OrbitSuccess
1994-08-27Titan 401A Centaur | Mercury 14Space Launch Complex 41Geostationary OrbitSuccess
1994-05-03Titan 401A Centaur | Trumpet 1Space Launch Complex 41Elliptical OrbitSuccess
1994-02-07Titan 401A Centaur | Milstar 1Space Launch Complex 40Geostationary OrbitSuccess

Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.

Further reading: Wikipedia