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Appendix a : Sea Launch System Components and System Integration, A. 1. 5

By Federal Aviation Administration

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Book Id: WPLBN0000665341
Format Type: PDF eBook
File Size: 62.25 KB
Reproduction Date: 2005

Title: Appendix a : Sea Launch System Components and System Integration, A. 1. 5  
Author: Federal Aviation Administration
Volume:
Language: English
Subject: Aviation, Federal Aviation Administration Command Center (U.S.), Mechanical engineering.
Collections: Space and Aviation eDocuments Collection
Historic
Publication Date:
Publisher: Federal Aviation Administration (FAA)

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Administration, F. A. (n.d.). Appendix a : Sea Launch System Components and System Integration, A. 1. 5. Retrieved from http://community.worldlibrary.org/


Excerpt
Excerpt: Three-axis stabilization of the Block DM-SL during coast periods is provided by two attitude control/ullage engines. Each engine has five nozzles that are grouped in clusters on either side of the main engine nozzle. The attitude control system uses the hypergolic propellants nitrogen tetroxide (N2O4) and monomethylhydrazine (MMH).

 

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