Martin Marietta Aerospace Corp. /NASA
Lockheed Martin Astronautics /USAF
Titan 2
(Gemini)
Titan 23G
Overall
Vehicle
Operational from 08.04.1964 05.09.1988

 

to 11.11.1966 18.10.2003
Orbital flights   13 13
Payload weight t LEO 3.80 SSO 1.50
Gross liftoff weight t 151.00 154.20
Gross propellant weight t 137.88 142.27
Total length m 32.94 35.60
Max. diameter (span) m 3.05 3.05
Total liftoff thrust (s.l.) kN 1,912.8 1,734.8
Total impulse (vac) MN*s 409.6 418.0

Fairing

Total length m 5.79 6.10/7.62/9.14
Diameter m 3.05 3.05
Total weight t 0.00 0.652/0.750/0.909
Stage 3

Name

    Star 37XFP
  Length m   1.50
Diameter m 3.05 (0.93)
Liftoff weight t 0.955
Propellant weight t 0.884
Engines  

TE-M-714-16

Propellant    solid HTPB
Total thrust (vac) kN 37.81
Specific impulse (vac) N*s/kg 2869
Burn time s  67.0
Total impulse (vac) MN*s 2.54

Stage 2

Name      
  Length m 5.76 6.59
Diameter m 3.05 3.05
Liftoff weight t 29.15 29.28
Propellant weight t 26.75 26.60
Engines   LR-91-AJ-7 LR-91-AJ-5
Propellant  

Aerozine 50/N2O4

Aerozine 50/N2O4

Total thrust (vac) kN 453.7 444.8
Specific impulse (vac) N*s/kg 3094 3094
Burn time s 182.5 185
Total impulse (vac) MN*s 82.8 82.3

Stage 1

Name      
  Length +interstage m 21.39 21.39
Diameter m 3.05 3.05
Liftoff weight t 118.05 121.71
Propellant weight t 111.13 114.79
Engines 2 LR-87-AJ-7 LR-87-AJ-5
Propellant  

Aerozine 50/N2O4

Aerozine 50/N2O4

Total thrust (s.l.) kN 1,912.8 1,734.8
Specific impulse (s.l.) N*s/kg 2432 2388
Burn time s 141.3 158
Total impulse (vac) MN*s 326.8 333.2