Earth escape trajectory from LEO. Code name: BravoSat. @benwl

Uploaded July 2013 | Updated September 2026, 1 week ago

Earth-escape trajectory for BravoSat mission using 200 W thrust maneuvers over 10 minutes at perigee (energetically feasible given other spacecraft parameters), exploiting the passive magnetic stabilization scheme resulting from the engine's permanent magnets. BravoSat starts in a 500 km by 1500 km polar orbit and escapes Earth in under 3 years with less than 1 kg of fuel (2.5 kg dry mass).

STK simulations and videos produced by: S. Spangelo. saraspangelo.com/consulting

http://pepl.engin.umich.edu/thrusters/CAT.html

Ongoing support provided by AGI: agi.com

S. C. Spangelo, B. W. Longmier, BravoSat: Optimizing the Delta-V Capability of a CubeSat Mission with Novel Plasma Propulsion Technology, Interplanetary Small Satellite Conference, Pasadena, CA, June 20-21, 2013

Earth escape trajectory from LEO. Code name: BravoSat.

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