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Titan IVB/Centaur

Titan familyLockheed MartinRetired

Titan IVB/Centaur vehicle

Specifications

Thrust
15,120 kN
Height
63 m
Diameter
3.05 m
Launch mass
943 t
Stages
3
LEO capacity
21,680 kg
GEO capacity
5,760 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

7flightswith a definitive outcome
85.7%success rate6 of 7
1failureincluding partial failures
4success streakcurrent

First flight October 15, 1997 · 08:43 UTC · latest September 9, 2003

Counted from padside's own launch record, the same basis as the stats page.

Flights per year

  • Successful
  • Failed
Show the numbers for Titan IVB flights per year
Titan IVB flights per year
YearSuccessfulFailedTotal
1997101
1998101
1999011
2000000
2001101
2002101
2003202

Flights

5 of 7

All 7 flights