SARGE | Launch 2 - "Mission 1"

Launch Vehicle

SARGE

Configuration:
Family: SARGE

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).

Suborbital

The SARGE rocket carried several small research payloads and was intended to reach a peak altitude of 80 kilometers. It only reached a peak altitude of about 20 kilometers before gliding back to a landing about 1.2 kilometers from the launch pad.