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- W2334359888 abstract "An RLV concept evolving over the last 16 years utilizes a pure lifting body shape (no wings). The configuration at launch weights about two million pounds and delivers about 10,000 pounds of payload to a polar orbit. The shape is dominated by the propellant tank, which is primary structure. In the planform view the tank is made up of a conical forebody and an afterbody consisting of a cylindrical three lobe Vee“. A unique feature, absent from other SSTO designs to date, is a conformal Crew capsule / Escape capsule which is an integral part of the conical forebody. The Crew capsule lifting body has the same geometry as the complete vehicle, except for the afterbody side surfaces, which are conical. For a near optimum trajectory to injection into a polar orbit at 50 NM miles, two engines (SSMES) can be shut down. This paper addresses the payload improvement by dropping these engines. In effect we are trading the saved propellant for payload and design improvements. This weight combination is more then doubled." @default.
- W2334359888 created "2016-06-24" @default.
- W2334359888 creator A5034016340 @default.
- W2334359888 date "2004-01-05" @default.
- W2334359888 modified "2023-09-26" @default.
- W2334359888 title "RLV Concept Employing Staged Rocket Engines" @default.
- W2334359888 cites W2333179717 @default.
- W2334359888 doi "https://doi.org/10.2514/6.2004-705" @default.
- W2334359888 hasPublicationYear "2004" @default.
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