@benwl
  @benwl
Plasma Ben | Earth escape trajectory from LEO. Code name: SierraSat. @benwl | Uploaded 11 years ago | Updated 11 minutes ago
Earth-escape trajectory for BravoSat mission with constant 10 W thrust maneuver along the velocity vector (energetically feasible given other spacecraft parameters). BravoSat starts in a 700 km circular polar orbit and escapes in under one year with 2.5 kg of fuel (2.5 kg dry mass).

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

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

Ongoing support provided by AGI: http://www.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: SierraSat.Flip MinoHD works in vacuum!A Private Astronauts Path to Space, Richard Garriott [HD]The known universeDrinking tea with chopsticks in microgravityQ&A: Future of Electric Propulsion III, Dr. Roald SagdeevSurface tension of water in microgravity 3Hubble Repair Mission 4, NOBL, HDHD: Hiking up to Grinell Glacier3D: How to take a group photo in ZeroGHubble Repair Mission 4, FGS, HDHD: Return to the Moon: lecture by Apollo Astronaut Dr. Schmitt

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

SHARE TO X SHARE TO REDDIT SHARE TO FACEBOOK WALLPAPER