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Apollo 9 mission report : supplement 5 : service propulsion system final flight evaluation.

Auteur : James Alton McDivitt; TRW Systems Group.; Manned Spacecraft Center (U.S.); United States. National Aeronautics and Space Administration.
Éditeur : Houston, Texas : National Aeronautics and Space Administration, Manned Spacecraft Center ; Springfield, Va. National Technical Information Service [distributor], 1969.
Édition/format :   Print book : Publication gouvernementale nationale : Anglais
Base de données :WorldCat
Résumé :
The purpose of this report is to present the results of the postflight analysis of the Service Propulsion System (SPS) performance during the Apollo 9 Mission. The primary objective of the analysis was to determine the steady-state performance of the SPS under the environmental conditions of actual space flight. This report has been prepared as Supplement 5 to the Apollo 9 Mission Report (EX-PA-R-69-2).
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Détails

Type d’ouvrage : Publication gouvernementale, Publication gouvernementale nationale, Ressource Internet
Format : Livre, Ressource Internet
Tous les auteurs / collaborateurs : James Alton McDivitt; TRW Systems Group.; Manned Spacecraft Center (U.S.); United States. National Aeronautics and Space Administration.
Numéro OCLC : 64383655
Notes : "December 1969."
"Prepared by TRW Systems; Approved by James A. McDivitt, Manager, Apollo Spacecraft Program."
"MSC-PA-R-69-2."
Notes de reproduction : Photocopy. Springfield, Va. : National Technical Information Service, 2000. 28 cm.
Description : iv, 72 pages : illustrations ; 28 cm
Responsabilité : prepared by TRW Systems.

Résumé :

The purpose of this report is to present the results of the postflight analysis of the Service Propulsion System (SPS) performance during the Apollo 9 Mission. The primary objective of the analysis was to determine the steady-state performance of the SPS under the environmental conditions of actual space flight. This report has been prepared as Supplement 5 to the Apollo 9 Mission Report (EX-PA-R-69-2).

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Données liées


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