|
VEHICLE OVERVIEW:
| |
LEO Payload
(28.7 deg.) |
Estimated Launch Price |
Configuration |
Launch Mass |
| X-38 |
N/A |
--- |
Single Stage -
Atmospheric and Re-Entry Test
Vehicle |
16,000 lb
7,250 kg |
VEHICLE CONFIGURATION:
| |
X-38 |
| Length |
28.5 ft
8.7 m |
| Width (wingspan) |
14.5 ft
4.4 m |
| Height |
--- |
| Gross Mass |
16,000 lb
7,250 kg |
Propellant
Propellant Mass (estimated) |
UDMH / N2O4
1,000 lb
455 kg |
Engine**
Thrust
Isp (estimated) |
TBD
3,500 lbf
15,540 N
335 sec |
| Number of Engines |
1 |
| Nominal Burn Time |
100 sec |
** Note: Vacuum engine performance unless
otherwise specified.
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