NEAR SPACECRAFT AND INSTRUMENTATION

Citation
Ag. Santo et al., NEAR SPACECRAFT AND INSTRUMENTATION, The Journal of the astronautical sciences, 43(4), 1995, pp. 373-397
Citations number
4
Categorie Soggetti
Aerospace Engineering & Tecnology
ISSN journal
00219142
Volume
43
Issue
4
Year of publication
1995
Pages
373 - 397
Database
ISI
SICI code
0021-9142(1995)43:4<373:NSAI>2.0.ZU;2-8
Abstract
The NEAR spacecraft design is mechanically simple, and geared toward a short development and test time. Except for the initial deployment of the solar panels and protective instrument covers, the spacecraft has only one moveable mechanism. A distributed architecture allows parall el development and test of each subsystem, yielding an unusually short spacecraft integration and test period. Several innovative features o f the NEAR design include the first use of an X-band solid state power amplifier for an interplanetary mission, the first use of a hemispher ical resonator gyroscope in space, and extremely high-accuracy high vo ltage power supply control. The spacecraft design enables exciting, fi rst-rate science return with low cost, quick turnaround, and low techn ical risk.