OTV orbital tanking systemsOrbital transfer of cryogenic propellants could benefit spacecraft and Orbital Transfer Vehicle (OTV) missions in the 1980s by supplying main propulsion, attitude control, or other fluid systems. The Space Shuttle can operate as a tanker when equipped with cryogenic propellant storage and orbital transfer systems. The key technologies are multilayer insulation, capillary propellant acquisition, zero-g gaging, orbital chilldown, and possibly large flight weight dewars. The technologies and operations could be realistically demonstrated using a Centaur that has been integrated with the Shuttle. Orbital refueling capability can enhance the usefulness of the whole Shuttle program
Document ID
19790054995
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Heald, D. A. (General Dynamics/Convair San Diego, CA, United States)
Merino, F. (General Dynamics Corp. Convair Div., San Diego, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1979
Subject Category
Space Transportation
Report/Patent Number
AIAA PAPER 79-1262Report Number: AIAA PAPER 79-1262
Meeting Information
Meeting: AIAA, SAE, and ASME, Joint Propulsion Conference