A de-orbiting system for a space vehicle may include one or more lithium ion (Li-ion) batteries configured to release hot gases to be used for thrusting during de-orbiting of the apparatus. The system may also include one or more heaters surrounding each of the one or more Li-ion batteries, which are configured to send each of the one or more Li-ion batteries into a thermal runaway. The thermal runaway causes the one or more Li-ion batteries to release stored electrochemical energy within each of the one or more Li-ion batteries.
Keywords: battery, lithium, thruster, de-orbit
International Class: B64G1/24, H01M10/0525, H01M10/615, B64G1/62, B64G1/26, B64G1/42, H01M50/30, H01M50/35