| タイトル | Base heating methodology improvements, volume 1 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930013161 |
| 著者（英） | Bender, Robert L.; Smith, Sheldon D.; Pergament, Harold; Somers, Richard E.; Fulton, Michael S.; Reardon, John E. |
| 著者所属（英） | Remtech, Inc. |
| 発行日 | 1992-11-01 |
| 言語 | eng |
| 内容記述 | This document is the final report for NASA MSFC Contract NAS8-38141. The contracted effort had the broad objective of improving the launch vehicles ascent base heating methodology to improve and simplify the determination of that environment for Advanced Launch System (ALS) concepts. It was pursued as an Advanced Development Plan (ADP) for the Joint DoD/NASA ALS program office with project management assigned to NASA/MSFC. The original study was to be completed in 26 months beginning Sep. 1989. Because of several program changes and emphasis on evolving launch vehicle concepts, the period of performance was extended to the current completion date of Nov. 1992. A computer code incorporating the methodology improvements into a quick prediction tool was developed and is operational for basic configuration and propulsion concepts. The code and its users guide are also provided as part of the contract documentation. Background information describing the specific objectives, limitations, and goals of the contract is summarized. A brief chronology of the ALS/NLS program history is also presented to provide the reader with an overview of the many variables influencing the development of the code over the past three years. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 93N22350
NASA-CR-192455
NAS 1.26:192455
RTR-218-01-VOL-1 |
| 権利 | No Copyright |
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