Earth escape trajectory from LEO. Code name: SierraSat. _v2

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. saraspangelo.co...
pepl.engin.umic....
Ongoing support provided by AGI: 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

[@jeffborders1146]

So you'd just constant velocity'd your way out. Lol. Hahaha. Where'd you find the fuel for that?