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Expendable LV's

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   Titan IVB - Specifications
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Vehicle Overview

Note:  Payload performance and estimated cost provided for information only.   If you are interested in contracting for launch services, we recommend that you contact the service provider directly using the information above.

  LEO 28.6° (150 x 175 km) LEO 90°
(185 km)
GSO Payload
(0° inclination)
Estimated Launch Price
Titan IV 405 NUS 47,800 lbm
21,680 kg
--- --- US $350 - 450 M
Titan I V 403 NUS --- 38,300 lbm
17,600 kg
--- US $350 - 450 M
Titan I V 401 Centaur --- --- 12,700 lbm
5,760 kg
US $350 - 450 M
Titan I V 402 IUS --- --- 5,250 lbm
2,380 kg
US $350 - 450 M

* Performance values from AIAA, "International Reference Guide to Space Launch Systems", 3rd edition. (NUS is no upper stage)

Vehicle Configuration

  SRMU Stage 1 Stage 2
Length 112.4 ft
34.3 m
86.5 ft
26.4 m
32.7 ft
10.0 m
Diameter 10.5 ft
3.2 m
10.0 ft
3.05 m
10.0 ft
3.05 m
Gross Mass 769,000 lbm
350,000 kg
359,000 lbm
163,000 kg
87,000 lbm
39,500 kg
Propellant
   Propellant Mass
88% HTPB
688,000 lbm
313,000 kg
N2O4/Aerozine-50
340,000 lbm
155,000 kg
N2O4/Aerozine-50
77,200 lbm
35,000 kg
Engine**
   Thrust
   Isp
SRMU
1,700,000 lbf
7,500 kN
285.6 sec
LR87-AJ-11
551,200 lbf
2,452 kN
302 sec
LR91-AJ-11
106,150 lbf
472,200 kN
316 sec
Number of Engines 2 2 1
Nominal Burn Time 137.8 sec 164 sec 223 sec

 

  Centaur IUS Stage 1 IUS Stage 2
Length 29.5 ft
9.0 m
11.5 ft
3.5 m
6.9 ft
2.1 m
Diameter 14 ft
4.3 m
7.7 ft
2.34 m
9.5 ft
2.9 m
Gross Mass 52,650 lbm
23,880 kg
24,040 lbm
10,900 kg
8,520 lbm
3,865 kg
Propellant
   Propellant Mass
LOX / LH2
46,185  lbm
20,950 kg
HTPB
21,580  lbm
9,790 kg
HTPB
6,060  lbm
2,750 kg
Engine**
   Thrust
   Isp
RL10A-3-3A
16,500 lbf
73,000 N
444 sec
SRM-1, Orbus 21
41,800 lbf
186,000 N
294 sec
SRM-2, Orbus 6E
17,200 lbf
76,500 N
EEC: 303.8 sec
w/o EEC: 289.6 sec 
Number of Engines 2 1 (1 segment) 1 (1 segment)
Nominal Burn Time 600 sec 153 sec 104 sec

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