Session
Technical Session III: Launch & Propulsion Systems
Abstract
Cubesats and other nano- and pico-satellite platforms have traditionally not had the capability of on-board propulsion. A complete propulsion system tailored to cubesat and other nano-picosat applications is presented in this paper. This system has been demonstrated and is ready for use in cubesat missions. A diaphragm positive expulsion tank or integral structure/bladder tank has been developed for propellant storage and feed to the thrusters. Propellant systems available include hydrogen peroxide, hydrazine or cold gas. Available thrust levels range from 5 to 100 milliNewtons. Power requirements are 0.5 watts and the voltage requirement is 12 volts.
Presentation Slides
A Propulsion System Tailored to Cubesat Applications
Cubesats and other nano- and pico-satellite platforms have traditionally not had the capability of on-board propulsion. A complete propulsion system tailored to cubesat and other nano-picosat applications is presented in this paper. This system has been demonstrated and is ready for use in cubesat missions. A diaphragm positive expulsion tank or integral structure/bladder tank has been developed for propellant storage and feed to the thrusters. Propellant systems available include hydrogen peroxide, hydrazine or cold gas. Available thrust levels range from 5 to 100 milliNewtons. Power requirements are 0.5 watts and the voltage requirement is 12 volts.
