Atomic hydrogen propellants - Historical perspectives and future possibilitiesAtomic hydrogen, a very high density free-radical propellant, is anticipated to generate a specific impulse of 600-1500 lb-f sec/lb-mass performance; this may facilitate the development of unique launch vehicles. A development status evaluation is presently given for atomic hydrogen investigations. It is noted that breakthroughs are required in the production, storage, and transfer of atomic hydrogen, before this fuel can become a viable rocket propellant.
Document ID
19930040237
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Palaszewski, Bryan (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Subject Category
Propellants And Fuels
Report/Patent Number
AIAA PAPER 93-0244Report Number: AIAA PAPER 93-0244
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit