Computer Science – Performance
Scientific paper
Nov 1993
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993jann....2..147h&link_type=abstract
In JHU, The 1993 JANNAF Propulsion Meeting, Volume 2 p 147-154 (SEE N95-16324 04-20)
Computer Science
Performance
Engine Design, Launch Vehicles, Propulsion, Propulsion System Configurations, Propulsion System Performance, Rocket Engine Design, Design Analysis, Lunar Landing Modules, Lunar Module Ascent Stage, Orbit Transfer Vehicles, Propellant Tanks, Systems Integration, Technology Assessment, Viking Lander Spacecraft
Scientific paper
Engine concepts characterized by modular architecture, advanced technologies, and enhanced operability applicability to a wide range of missions (i.e., upper stage, space-based, transfer, lunar lander, ascent, and Mars lander propulsion systems). Two widely different propulsion system applications, a launch vehicle upper stage and a lunar lander vehicle, were developed around a common propulsion system architecture. These Integrated Modular Engine (IME) systems include propellant tanks, propellant distribution, and the rocket engines. This approach focused on automating and minimizing operations required for preparing and placing a propulsion system into operation. The versatility of the IME system architecture is described along with options to further integrate stage or vehicle functions.
Briley G. L.
Harmon Timothy J.
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