McDonnell Douglas / APL / Honeywell / Jet Propulsion Laboratory / O PSV1 OPSV2 FPSV1 F BV / Power System Electronics / Motorola / V DC Bus Shunts Power System Electronics / The Johns Hopkins University Applied Physics Laboratory / /
Currency
ILS / AED / /
Facility
POWER SUBSYSTEM The power system / Terminal Boards / Jet Propulsion Laboratory / /
IndustryTerm
software-defined interfaces / normal communications / low conductivity mounting hardware / coaxial switching network / launch site / system electronics / direct energy transfer system / positive gas-free expulsion / gas-free propellant / electronics / command/telemetry processors / in-line propulsion management devices / energy / /
MusicGroup
Interface / /
Organization
The Johns Hopkins University / African Union / Data Bus Command / Attitude Interface Unit Flight Computers Command / Data Handling Command / Cassini mission / National Aeronautics and Space Administration / Ray Data Processor Unit / Data Bus Star Camera Flight Computer Low Gain Antennas Pwr Amp Diplexer X-Band Transponder Command / /
Person
Ray Spectrometer / /
Position
idiz er PM / Solar Panel Forward / /
ProvinceOrState
Maryland / /
Technology
Laser / seven processors / coaxial cable / X-Ray / Deep Space Network / condensation / 1553 Data Bus Command/ Telemetry Processor / 1553 Data Bus Star Camera Flight Computer Low Gain Antennas Pwr Amp Diplexer X-Band Transponder Command/ Telemetry Processor / command/telemetry processors / /
NEAR SPACECRAFT AND INSTRUMENTATION1 A. G. Santo, S. C. Lee, and R. E. Gold The NEAR spacecraft design is mechanically simple, and geared toward a short