The performance characteristics and mission capabilities of the nuclear rocket engine.
Nuclear rocket engine design for near-optimum vehicle performance for mission capability
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Nuclear rocket engine design for near-optimum vehicle performance for mission capability
Nuclear and explosive destruct concepts for nuclear rocket engines
Nuclear rocket research and development was initiated in the United States in 1955 and is still being pursued to a limited extent. The major technology emphasis occurred in the decade of the 1960s and was primarily associated with the Rover/NERVA Program where the technology for a nuclear rocket engine system for space application was developed and demonstrated. The NERVA (Nuclear Engine for Rocket Vehicle Application) technology developed twenty years ago provides a comprehensive and viable propulsion technology base that can be applied and will prove to be valuable for application to the NASA Space Exploration Initiative (SEI). This paper, which is historical in scope, provides an overview of the conduct of the NERVA Engine Program, its organization and management, development philosophy, the engine configuration, and significant accomplishments.
Nuclear rocket research and development was initiated in the United States in 1955 and is still being pursued to a limited extent. The major technology emphasis occurred in the decade of the 1960s and was primarily associated with the Rover/NERVA Program where the technology for a nuclear rocket engine system for space application was developed and demonstrated. The NERVA (Nuclear Engine for Rocket Vehicle Application) technology developed twenty years ago provides a comprehensive and viable propulsion technology base that can be applied and will prove to be valuable for application to the NASA Space Exploration Initiative (SEI). This paper, which is historical in scope, provides an overview of the conduct of the NERVA Engine Program, its organization and management, development philosophy, the engine configuration, and significant accomplishments.
Specific nuclear light bulb and open-cycle vortex stabilized gaseous nuclear rocket engine designs
Controls and control experimental program for nuclear rocket engine employing hot bleed cycle
Parameter adjustment model reference adaptive control of nuclear rocket engine, noting design parameters, system performance, propellant savings estimates and dynamic stability
Moderator wall cooling of high thrust cavity type gaseous nuclear rocket engines
Noise spectra in nuclear rocket engine ground test
NERVA nuclear rocket engine for space propulsion and long duration auxiliary power generation
An initial investigation of the design considerations in clustering nuclear rocket engines for space transfer vehicles has been made. The clustering of both propulsion modules (which include start tanks) and nuclear rocket engines installed directly to a vehicle core tank appears to be feasible. Special provisions to shield opposite run tanks and the opposite side of a core tank - in the case of the boost pump concept - are required; the installation of a circumferential reactor side shield sector appears to provide an effective solution to this problem. While the time response to an engine-out event does not appear to be critical, the gimbal displacement required appears to be important. Since an installation of three engines offers a substantial reduction in gimbal requirements for engine-out and it may be possible to further enhance mission reliability with the greater number of engines, it is recommended that a cluster of four engines be considered.
Liquid hydrogen flow system startup of full scale simulated nuclear rocket engine
Noise field from ground testing of nuclear rocket engines operated at various reactor power levels
Linear stability of nuclear rocket engines with two reactivity feedbacks in core
Effect of fuel opacity on temperature distribution in gaseous nuclear rocket engine
Performance potential of radiant heat transfer liquid-core nuclear rocket engine
Cold flow startup test on nuclear rocket engine using radial turbopump
Design, development, and characteristics of open cycle, gas core nuclear rocket engine