SARGE

Active Re-Usable

EXOS 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
    ―

EXOS Aerospace

Commercial
President: David Mitchell
EXOS 2014

Exos 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.


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