TRW Inc. has opened a new electric propulsion test facility designed to enhance the company's role in the implementation of this technology for spacecraft applications. The Cryogenic Electric Propulsion Test Stand (CEPTS) at TRW's Space Park facility contains state-of-the-art equipment that will be used to optimize electric thruster designs, perform in-house testing of integrated systems, and support customer-funded testing.

"Electric propulsion is an industry-recognized key discriminator

for some satellite systems," said Mary Kriebel, TRW manager for the

Propulsion Systems Engineering section. "Recent improvements in space

power systems have made electric propulsion feasible, and the fuel

efficiency of electric propulsion makes these systems highly

desirable.

"The demand for electric propulsion systems is growing rapidly in

the coming decades, especially for telecommunications satellites,"

Kriebel added. "CEPTS is a key ingredient in keeping TRW on top of,

and competitive with, evolving electric propulsion technology."

CEPTS was developed to provide the space-like vacuum conditions

necessary for testing various electric propulsion thrusters, such as

Hall Effect Thrusters and pulsed plasma thrusters. The facility

features a test cell approximately 7 feet in diameter and 17 feet

long, and has three 48-inch cryogenic vacuum pumps to allow the

chamber to maintain very high vacuum levels while a thruster is

operating.

The company-funded facility is also being outfitted with an

autonomous data acquisition and control system that will allow

unmanned operation and data collection during long-duration testing.

System life testing can demand in excess of 5,000 hours, requiring

automation in test control and data acquisition. Opened last month,

the facility operated successfully the first time it performed

thruster testing.

Electric thrusters have much higher specific impulse than

chemical thrusters, and provide two to three times more fuel

efficiency than chemical thrusters. Higher fuel efficiency means that

not as much propellant is needed on-board, allowing spacecraft

designers to reduce overall spacecraft weight and launch costs or to

add more weight and capability to the payload.

Electric propulsion is applicable for multiple types of in-space

missions, ranging from inserting spacecraft into specific orbits to

repositioning spacecraft, stationkeeping, constellation management,

and on occasion, deorbitting a spacecraft.

TRW has conducted electric propulsion research and development

for many years. Under Air Force funding, TRW headed an industrial team

that delivered a flight arcjet system for integration onto the Air

Force's Advanced Research and Global Observation Satellite. TRW is now

conducting sponsored and internally-supported efforts to develop

selected electric propulsion technologies.