SARGE
Active Re-UsableEXOS Aerospace (EXOS)
Aug. 25, 2018
Description
The SARGE vehicle is based on the STIG B platform developed as part of Armadillo Aerospace's lunar lander program. The SARGE vehicle employs a LOX-ethanol propulsion module based on the LE23000FC series engines, producing approximately 5500 lbs of thrust. The airframe is a reusable sounding rocket with a 20 inches (51 cm) diameter, and is 36 feet (11 m) tall. Helium pressurant cold gas thrusters provide attitude control for pitch-roll-yaw and pointing capability. Payload must fit inside a 20 inches (51 cm) diameter cylinder, be no more than 36 inches (91 cm) tall (in its standard configuration) and weigh no more than 50 kilograms (110 lb).
Specifications
-
Stages
1 -
Length
11.0 m -
Diameter
0.51 m -
Fairing Diameter
― -
Launch Mass
― -
Thrust
24.0 kN -
Apogee (Sub-Orbital)
80.0 km
Family
-
Name
SARGE -
Family
― -
Variant
― -
Alias
― -
Full Name
SARGE
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
― -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
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EXOS Aerospace
Commercial
President: David Mitchell
EXOS 2014Exos Aerospace Systems & Technologies is an aerospace manufacturer and developer of reusable launch systems intended to support unmanned orbital spaceflight launches, and is based in Caddo Mills, Texas.
Flight Record
No spaceflights found for .
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