| タイトル | Cryogenic Propellant Storage and Transfer Technology Demonstration: Prephase A Government Point-of-Departure Concept Study |
| 本文（外部サイト） | http://hdl.handle.net/2060/20120016527 |
| 著者（英） | Capizzo, P. D.; Thomas, H. D.; Hornsby, L. S.; Gwaltney, D. A.; Addona, B. M.; Mulqueen, J. A.; Matis, J. A.; Baysinger, M. F.; Hopkins, R. C.; Percy, T. K.; Maples, C. D.; Thomas, S. D.; McRight, P. S.; Fabisinski, L. L.; Sutherlin, S. G.; Popp, C. G.; Holt, K. A. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2012-09-01 |
| 言語 | eng |
| 内容記述 | The primary purpose of this study was to define a point-of-departure prephase A mission concept for the cryogenic propellant storage and transfer technology demonstration mission to be conducted by the NASA Office of the Chief Technologist (OCT). The mission concept includes identification of the cryogenic propellant management technologies to be demonstrated, definition of a representative mission timeline, and definition of a viable flight system design concept. The resulting mission concept will serve as a point of departure for evaluating alternative mission concepts and synthesizing the results of industry- defined mission concepts developed under the OCT contracted studies |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | NASA/TM-2012-217467
M-1343 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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