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The ram accelerator - A chemically driven mass launcherThe ram accelerator, a chemically propelled mass driver, is presented as a viable new approach for directly launching acceleration-insensitive payloads into low earth orbit. The propulsion principle is similar to that of a conventional air-breathing ramjet. The cargo vehicle resembles the center-body of a ramjet and travels through a tube filled with a pre-mixed fuel and oxidizer mixture. The launch tube acts as the outer cowling of the ramjet and the combustion process travels with the vehicle. Two drive modes of the ram accelerator propulsion system are described, which when used in sequence are capable of accelerating the vehicle to as high as 10 km/sec. The requirements are examined for placing a 2000 kg vehicle into a 500 km orbit with a minimum of on-board rocket propellant for circularization maneuvers. It is shown that aerodynamic heating during atmospheric transit results in very little ablation of the nose. An indirect orbital insertion scenario is selected, utilizing a three step maneuver consisting of two burns and aerobraking. An on-board propulsion system using storable liquid propellants is chosen in order to minimize propellant mass requirements, and the use of a parking orbit below the desired final orbit is suggested as a means to increase the flexibility of the mass launch concept. A vehicle design using composite materials is proposed that will best meet the structural requirements, and a preliminary launch tube design is presented.
Document ID
19880057896
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kaloupis, P.
(Washington Univ. Seattle, WA, United States)
Bruckner, A. P.
(Washington, University Seattle, United States)
Date Acquired
August 13, 2013
Publication Date
July 1, 1988
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 88-2968
Accession Number
88A45123
Funding Number(s)
CONTRACT_GRANT: NAG1-746
Distribution Limits
Public
Copyright
Other

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