Presentation 1997/6/27
Missions on Lagrange's Orbit, Earth-Drift Orbit, and Earth-Rendezvous Orbit
Masayoshi Utashima,
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Abstract(in Japanese) (See Japanese page)
Abstract(in English) Several orbits suitable for new space missions such as advanced space telescopes are described. Advanced infrared space telescope requires circumstances that enable low temperature and long integration time. L2 point in the Sun-Earth system is adequate for this mission, because the effect of the Earth's albedo is negligible and the Sun and Earth, which are obstacles to the observation, exist only one direction from the L2 point. The L2 point is also adequate for the optical interferometer that requires small gravity gradient. For the detection of all the NEOs (Near Earth Object) larger than 100m diameter, several telescopes on the Lagrange's points, Earth-Drift Orbit, and Earth-Rendezvous Orbit are effective.
Keyword(in Japanese) (See Japanese page)
Keyword(in English) Lagrange's Points / Earth-Drift Orbit / Earth-Rendezvous Orbit / SpaceGuard / Optical Interferometer / Near Earth Object
Paper # SANE97-26
Date of Issue

Conference Information
Committee SANE
Conference Date 1997/6/27(1days)
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Paper Information
Registration To Space, Aeronautical and Navigational Electronics (SANE)
Language JPN
Title (in Japanese) (See Japanese page)
Sub Title (in Japanese) (See Japanese page)
Title (in English) Missions on Lagrange's Orbit, Earth-Drift Orbit, and Earth-Rendezvous Orbit
Sub Title (in English)
Keyword(1) Lagrange's Points
Keyword(2) Earth-Drift Orbit
Keyword(3) Earth-Rendezvous Orbit
Keyword(4) SpaceGuard
Keyword(5) Optical Interferometer
Keyword(6) Near Earth Object
1st Author's Name Masayoshi Utashima
1st Author's Affiliation Advanced Mission Research Center, National Space Development Agenry of Japan()
Date 1997/6/27
Paper # SANE97-26
Volume (vol) vol.97
Number (no) 142
Page pp.pp.-
#Pages 7
Date of Issue