Effects of propulsion system characteristics on ascent performance of dual-fueled single-stage earth-to-orbit transports
By: John J. Rehder.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Series: NASA technical paper ; 1115; NASA technical paper -- 1115.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1977
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 63
Subjects: Space vehicles -- Propulsion systems.
Notes: Issued Dec. 1977.

Includes bibliographical references.