ApolloTechnical Memorandum (TM)
Utilization and characteristic velocity saving with a small throttleable region about 92.5 per cent thrust for LM powered descent
20191 min read16 words
Mc Swain, G. G. and Moore, T. E.
Legacy CDMS
Utilizing small throttling capability about high thrust region of 92.5 % for lunar module powered descent
Related Apollo Documents
Apollo
A Flexible Lunar Architecture for Exploration (FLARE) Supporting NASA’s Artemis Program
The Flexible Lunar Architecture for Exploration (FLARE) is a concept to deliver four crew to the lunar surface for a minimum of seven days and then return them safely to Earth. FLARE can be implemente
2020·Reprint (Version printed in journal)
ApolloA historical overview of the electrical power systems in the US manned and some US unmanned spacecraft
A historical overview of electrical power systems used in the U.S. manned spacecraft and some of the U.S. unmanned spacecraft is presented in this investigation. A time frame of approximately 25 years
2019·Contractor Report (CR)
ApolloA Notional Artemis Lunar Surface Exploration Package (ArLSEP) based on the Gandalf Staff Platform
Introduction: The Artemis program is planning to deliver crew and cargo to the lunar surface, but there is no current package for supporting lunar in-struments and experiments similar to the Apollo L
2022·Conference Paper