# US 5,352,861 A · Resonant high-voltage pulser for arcjet thruster ignition

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- Number: US 5,352,861 A
- Document ID: US5352861A
- Status: Granted
- Kind: A
- Application number: 07/955,970
- Filed: 1992-10-02
- Granted: 1994-10-04
- Earliest claimed: 1992-10-02
- Assignees: General Electric Company
- Inventors: Robert L. Steigerwald; John N. Park
- Web page: https://patentgrep.com/patent/US5352861A

## CPC

- H02M 1/36: Means for starting or stopping converters
- B64G 1/415: {Arcjets or resistojets}
- B64G 1/428: {Power distribution and management}
- 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)}
- F03H 1/0018: {Arrangements or adaptations of power supply systems (for cosmonautic vehicles B64G1/42)}
- H02M 3/3376: {with automatic control of output voltage or current}
- 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
- H02M: APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF (transformers H01F; dynamo-electric converters H02K47/00; controlling transformers, reactors or choke coils, control or regulation of electric motors, generators or dynamo-electric converters H02P)
- B64G: COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- F03H: PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR (from combustion products F02K)
- Y02B: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS

## Abstract

A starting circuit for providing a high-voltage pulse for igniting an arc in an arcjet thruster includes a resonant capacitor for storage of the energy required to generate the high-voltage pulse. The capacitor is resonantly switched with a small resonant inductor which, in turn, resonates with a high-voltage cable capacitance, generating a high-voltage pulse via a step-up transformer to the arcjet thruster for igniting the arc. Advantageously, the transformer turns ratio is minimized, thus minimizing the required transformer size and weight; and the high-voltage pulse is isolated from the arcjet power supply semiconductor devices.

## Claims

### Claim 1

A power supply for a thruster, comprising a thruster:
a power converter for providing an ac voltage;
a rectifier coupled at the output of said converter for rectifying said ac voltage;
an output filter inductor connected to said rectifier for smoothing current supplied to said thruster, said filter inductor comprising a secondary winding of a step-up transformer;
a resonant starting circuit comprising a primary winding of said transformer, a resonant inductance, a storage capacitance, the capacitance of a cable means coupling said filter inductor to said thruster, and switching means, said switching means being activated to release energy stored in said storage capacitance such that the capacitance of said cable means resonates with said inductance and generates a starting pulse to said primary winding, said starting pulse being stepped-up in voltage via said transformer and applied to said thruster for ignition thereof.

### Claim 2 (depends on 1)

The power supply of claim 1 wherein said inductance comprises the leakage inductance of said transformer.

### Claim 3 (depends on 1)

The power supply of claim 1 wherein said transformer is situated on the same end of said cable as said thruster.

### Claim 4 (depends on 1)

The power supply of claim 1 wherein said thruster comprises an arcjet thruster.

### Claim 5

A resonant starting circuit for a thruster, comprising a thruster:
a resonant inductance, a storage capacitance, and the capacitance of a cable coupling a thruster power supply to said thruster, coupled to each other;
a primary winding of a step-up transformer for coupling said resonant inductance and said storage capacitance to said thruster;
switching means for releasing energy stored in said storage capacitance upon activation thereof such that the capacitance of said cable means resonates with said inductance and generates a starting pulse to said primary winding, said starting pulse being stepped-up in voltage via said transformer and applied to said thruster for ignition thereof.

### Claim 6 (depends on 5)

The starting circuit of claim 5 wherein said inductance comprises the leakage inductance of said transformer.

### Claim 7 (depends on 5)

The starting circuit of claim 5 wherein said transformer is situated on the same end of said cable as said thruster.

### Claim 8 (depends on 5)

The starting circuit of claim 5 wherein said thruster comprises an arcjet thruster.