Information for "Engineering:Descent Propulsion System"

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Display title	Engineering:Descent Propulsion System
Default sort key	Descent Propulsion System
Page length (in bytes)	11,819
Namespace ID	3034
Namespace	Engineering
Page ID	262182
Page content language	en - English
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Page creator	imported>JMinHep
Date of page creation	22:53, 15 March 2024
Latest editor	imported>JMinHep
Date of latest edit	22:53, 15 March 2024
Total number of edits	1
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Description	Content
Article description: (`description`) This attribute controls the content of the `description` and `og:description` elements.	The Descent Propulsion System (DPS) or Lunar Module Descent Engine (LMDE) is a variable-throttle hypergolic rocket engine developed by Space Technology Laboratories (TRW) for use in the Apollo Lunar Module Descent Stage. It used Aerozine 50 fuel and dinitrogen tetroxide (N2O4) oxidizer. This engine used...

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