HUGHES SPACE AND TELECOMMUNICATIONS COMPANY
Electron Dynamics Division
P.O. Box 92919 (S10/S323)
Los Angeles, CA 90009
Public Relations (310) 364-6363
Investor Relations (310) 662-9688
HUGHES' ION PROPULSION SYSTEM TO DRIVE NASA'S DEEP SPACE 1
TORRANCE, Calif., Oct. 19, 1998 -- The ion engines "Star Trek's" Mr.
Spock dreamt of 30 years ago are now a reality. When NASA's Deep
Space 1 spacecraft is launched from Cape Canaveral this month, it will
carry a revolutionary ion propulsion system designed with NASA and
manufactured by Hughes Electron Dynamics Division, a unit of Hughes
Electronics Corporation.
The NASA Solar Electric Power Technology Application Readiness
(NSTAR) 30-centimeter system, consisting of an ion thruster, power
processor, and digital control and interface units, was designed
specifically to support NASA's future requirements. It is being
validated by the New Millennium Deep Space 1 project. Unlike its
commercial satellite counterpart that uses a xenon ion propulsion
system, XIPS (pronounced "zips"), for north-south stationkeeping and
for orbit raising, the NSTAR system will be the primary propulsion
system for the Deep Space 1 spacecraft.
The Deep Space 1 spacecraft may be the first of several to use the
NSTAR system. Under the $8.1 million contract that was awarded by
NASA to Hughes Electron Dynamics Division in 1995, two flight
thrusters, and associated power processor and digital control and
interface units, were produced.
The advantage of ion propulsion is efficiency. Ion propulsion is
10 times more efficient than chemical thrusters. This translates into
a reduction of propellant mass of up to 90%. For commercial
communications satellites, the reduced propellant mass creates an
option to reduce launch cost, increase payload, or increase satellite
lifetime, or any combination of the above.
For Deep Space 1, the improved propellant efficiency of the NSTAR
system results in a lighter spacecraft that will reach its destination
in half the time. Deep Space 1 is currently scheduled to reach the
near-Earth asteroid 1992 KD in July 1999. By Oct. 1999, Deep Space 1
will have completed its primary mission and will be on a trajectory
that could result in an encounter with Comets Wilson-Harrington and
Borelly in 2001.
"XIPS is the result of more than 40 years of research by Hughes and
NASA. The NSTAR 30-centimeter system was designed to meet very
specific operational parameters," said Tim Fong, manager of Hughes
Electron Dynamics Division. "The NSTAR ion propulsion system on Deep
Space 1 requires operation over a wide range of thrust and input
power, since the solar power available drops significantly as the
spacecraft goes further away from the sun. This NSTAR system is
remotely programmable, allowing NASA to adjust its thrust to meet
these changing conditions over the life of the mission."
In addition to the 30-centimeter NSTAR system designed for NASA,
Hughes Electron Dynamics Division also produces two commercial XIPS
systems: a 13-centimeter unit that is an option on the HS 601
spacecraft built by Hughes Space and Communications Company, and a
25-centimeter version that will debut on Hughes' first HS 702 in early
1999.
Hughes Electron Dynamics Division built the first commercial XIPS
system, which was launched Aug. 28, 1997, on PAS-5, an HS 601HP
satellite for PanAmSat Corporation.
Hughes Electron Dynamics Division is a world leader in the design
and manufacture of microwave, traveling wave-tube amplifiers, and ion
thrusters for commercial and military applications. The earnings of
Hughes Electronics are used to calculate the earnings per share
attributable to GMH (NYSE symbol) common stock.