NEAR MISSION OVERVIEW AND TRAJECTORY DESIGN

Citation
Rw. Farquhar et al., NEAR MISSION OVERVIEW AND TRAJECTORY DESIGN, The Journal of the astronautical sciences, 43(4), 1995, pp. 353-371
Citations number
18
Categorie Soggetti
Aerospace Engineering & Tecnology
ISSN journal
00219142
Volume
43
Issue
4
Year of publication
1995
Pages
353 - 371
Database
ISI
SICI code
0021-9142(1995)43:4<353:NMOATD>2.0.ZU;2-B
Abstract
The Near-Earth Asteroid Rendezvous (NEAR) mission will be the first la unch in NASA's new series of low-cost planetary missions called the Di scovery Program. In February 1996, a Delta-2 rocket will place NEAR in to a two-year Delta VEGA trajectory that will eventually rendezvous wi th the large near-Earth asteroid 433 Eros. The initial close pass at E ros (distance similar to 500 km) will occur on February 6, 1999. Later , as the spacecraft is maneuvered closer to Eros, NEAR will conduct sc ience operations from orbits as low as 35 x 35 km. On its way to Eros, NEAR will perform a flyby of the main-belt asteroid 253 Mathilde on J une 27, 1997. Among its many spaceflight ''firsts,'' NEAR will be the first spacecraft to orbit a small body.