Resonant power supply for an arcjet thruster

• US 5,414,238 A
• Filed: 10/02/1992
• Issued: 05/09/1995
• Est. Priority Date: 10/02/1992
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Martin Marietta Corporation
• Inventors: Steigerwald, Robert L., Park, John N.
• Primary Examiner(s): Paschall, Mark H.
• Application Number:
  US07/956,130
• Time in Patent Office: 949 Days
• Field of Search: 219/121.43, 219/121.54, 219/121.48, 219/121.57, 219/130.4, 60/203.1, 363/26, 363/37, 363/17
• US Class Current: 219/121.54
• CPC Class Codes: B64G 1/415 Arcjets or resistojets
• CPC Class Codes: B64G 1/428 Power distribution and management
• CPC Class Codes: F03H 1/00 Using plasma to produce a reactive propulsive thrust generating plasma H05H1/00 ion sources per se H01J27/02, ion sources for plasma processing or ion beams H01J37/08
• CPC Class Codes: F03H 1/0018 Arrangements or adaptations of power supply systems for cosmonautic vehicles B64G1/42
• CPC Class Codes: H02M 3/3376 with automatic control of output voltage or current
• CPC Class Codes: Y02B 70/10 Technologies improving the efficiency by using switched-mode power supplies [SMPS], i.e. efficient power electronics conversion e.g. power factor correction or reduction of losses in power supplies or efficient standby modes

Abstract

A power supply for a thruster for space applications (e.g., an arcjet thruster) comprises a series/parallel resonant converter wherein the load quality (Q) factor of the resonant tank circuit inherently varies with arc voltage so as to accommodate changes in arc voltage from initiation thereof through steady-state operation. Effectively, the resonant tank circuit acts as a ballast by matching the arc during initiation thereof through steady-state operation. Furthermore, the resonant converter operates in a soft-switching, low-voltage switched mode so as to maximize efficiency.

Claims

1. A power supply for a thruster, comprising:

a full-bridge resonant converter including a resonant tank circuit for stabilizing the load of said thruster; and

control means for regulating the output current of said resonant converter substantially independent of an output voltage, the load quality factor of said resonant tank circuit varying in accordance with said output voltage and said output current so as to operate in a predetermined steady-state operating range, said steady-state operating range extending from a relatively low output voltage and a relatively high output current to a relatively high output voltage and a low output current.

2. The power supply of claim 1 wherein said control means comprises:

frequency control means for adjusting the operating frequency of said resonant converter in response to an error current, said error current comprising the difference between a commanded current and the arc current; and

phase control for phase shifting the voltage of each leg of the full-bridge with respect to the other in order to control the voltage applied to said resonant tank circuit.