Spacecraft velocity change maneuvers by variable arcjets

Abstract

A spacecraft uses monopropellant arcjets for velocity change such as for north-south stationkeeping. It has been discovered that, while an arcjet cannot be modulated by pulsing the fuel supply, the amount of thrust can be varied by modulating the power applied to the arc, without extinguishing the arc. While the specific impulse (I.sub.SP) of the arcjet is thereby reduced from the maximum I.sub.SP of which the arcjet is capable, the resulting I.sub.SP may still be larger than the combined I.sub.SP of an unmodulated arcjet in conjunction with a modulated chemical thruster in a typical scenario. According to the invention, attitude control is provided in conjunction with north-south stationkeeping or other velocity change by, in response to an error signal generated by an attitude control system, modulating the arc power(s) of an arcjet thruster(s), which provides the velocity change. The arc is not extinguished during the stationkeeping maneuver, but is varied in magnitude. In addition to improving the overall I.sub.SP, an arrangement according to the invention allows dispensing with the chemical thrusters on the north face, thereby reducing spacecraft weight and complexity. Reliability is not seriously affected, because failure of arc allows an arcjet to continue to be used as a chemical thruster.

Dependencies are inferred from the claim text.