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) |
SSO
(260 X 800 km, 98.6°) |
Estimated Launch Price |
| Titan II |
--- |
4200
lbm
1900 kg |
2425
lbm
1100 kg |
US
$30-40 M |
* Performance values
from AIAA, "International Reference Guide to Space Launch
Systems", 3rd edition.
Vehicle Configuration
| |
Stage 1 |
Stage
2 |
| Length |
70.7 ft
21.5 m |
24 ft
7.3 m |
| Diameter |
10.0 ft
3.05 m |
10.0 ft
3.05 m |
| Gross Mass |
269,000 lbm
122,018 kg |
65,000 lbm
30,000 kg |
Propellant
Propellant Mass |
N2O4/Aerozine-50
260,000 lbm
118,000 kg |
N2O4/Aerozine-50
59,000 lbm
27,000 kg |
Engine**
Thrust
Isp |
LR87-AJ-5
474,000 lbf
2,092 kN
296 sec |
LR91-AJ-5
100,000 lbf
440 kN
316 sec |
| Number of Engines |
2 |
1 |
| Nominal Burn Time |
147 sec |
182 sec |
|
