Suess-Urey mission (return of solar matter to Earth)

Donald Rapp; Firouz Naderi; Marcia Neugebauer; Donald Sevilla; Donald Sweetnam; Donald Burnett; Roger Wiens; Nicholas Smith; Benton Clark; David McComas; Eileen Stansbery

doi:10.1016/S0094-5765(96)00140-3

Suess-Urey mission (return of solar matter to Earth)

Donald Rapp, Firouz Naderi, Marcia Neugebauer, Donald Sevilla, Donald Sweetnam, Donald Burnett, Roger Wiens, Nicholas Smith, Benton Clark, David McComas, Eileen Stansbery

Research output: Contribution to journal › Conference article

6 Scopus citations

Abstract

The Suess-Urey (S-U) mission has been proposed as a NASA Discovery mission to return samples of matter from the Sun to the Earth for isotopic and chemical analyses in terrestrial laboratories to provide a major improvement in our knowledge of the average chemical and isotopic composition of the solar system. The S-U spacecraft and sample return capsule will be placed in a halo orbit around the L1 Sun-Earth libration point for two years to collect solar wind ions which implant into large passive collectors made of ultra-pure materials. Constant Spacecraft-Sun-Earth geometries enable simple spin stabilized attitude control, simple passive thermal control, and a fixed medium gain antenna. Low data requirements and the safety of a Sun-pointed spinner, result in extremely low mission operations costs.

Original language	English (US)
Pages (from-to)	229-238
Number of pages	10
Journal	Unknown Journal
Volume	39
Issue number	1-4
DOIs	https://doi.org/10.1016/S0094-5765(96)00140-3
State	Published - Jan 1 1996
Externally published	Yes
Event	Proceedings of the 1996 2nd IAA International Conference on Low-Cost Planetary Missions - Laurel, MD, USA Duration: Apr 16 1996 → Apr 19 1996

All Science Journal Classification (ASJC) codes

Aerospace Engineering

Access to Document

10.1016/S0094-5765(96)00140-3

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Rapp, D., Naderi, F., Neugebauer, M., Sevilla, D., Sweetnam, D., Burnett, D., Wiens, R., Smith, N., Clark, B., McComas, D., & Stansbery, E. (1996). Suess-Urey mission (return of solar matter to Earth). Unknown Journal, 39(1-4), 229-238. https://doi.org/10.1016/S0094-5765(96)00140-3

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abstract = "The Suess-Urey (S-U) mission has been proposed as a NASA Discovery mission to return samples of matter from the Sun to the Earth for isotopic and chemical analyses in terrestrial laboratories to provide a major improvement in our knowledge of the average chemical and isotopic composition of the solar system. The S-U spacecraft and sample return capsule will be placed in a halo orbit around the L1 Sun-Earth libration point for two years to collect solar wind ions which implant into large passive collectors made of ultra-pure materials. Constant Spacecraft-Sun-Earth geometries enable simple spin stabilized attitude control, simple passive thermal control, and a fixed medium gain antenna. Low data requirements and the safety of a Sun-pointed spinner, result in extremely low mission operations costs.",

author = "Donald Rapp and Firouz Naderi and Marcia Neugebauer and Donald Sevilla and Donald Sweetnam and Donald Burnett and Roger Wiens and Nicholas Smith and Benton Clark and David McComas and Eileen Stansbery",

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T1 - Suess-Urey mission (return of solar matter to Earth)

AU - Rapp, Donald

AU - Naderi, Firouz

AU - Neugebauer, Marcia

AU - Sevilla, Donald

AU - Sweetnam, Donald

AU - Burnett, Donald

AU - Wiens, Roger

AU - Smith, Nicholas

AU - Clark, Benton

AU - McComas, David

AU - Stansbery, Eileen

PY - 1996/1/1

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AB - The Suess-Urey (S-U) mission has been proposed as a NASA Discovery mission to return samples of matter from the Sun to the Earth for isotopic and chemical analyses in terrestrial laboratories to provide a major improvement in our knowledge of the average chemical and isotopic composition of the solar system. The S-U spacecraft and sample return capsule will be placed in a halo orbit around the L1 Sun-Earth libration point for two years to collect solar wind ions which implant into large passive collectors made of ultra-pure materials. Constant Spacecraft-Sun-Earth geometries enable simple spin stabilized attitude control, simple passive thermal control, and a fixed medium gain antenna. Low data requirements and the safety of a Sun-pointed spinner, result in extremely low mission operations costs.

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T2 - Proceedings of the 1996 2nd IAA International Conference on Low-Cost Planetary Missions

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