Operational safety of nuclear rockets.
Nuclear rocket operational safety analysis to protect operations personnel and public from radiation and falling objects
SEARCH · Search NASA
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Nuclear rocket operational safety analysis to protect operations personnel and public from radiation and falling objects
Nuclear light bulb and coaxial flow gaseous core nuclear rocket reactors based on energy transfer via thermal radiation
Nuclear rocket propulsion development, noting nuclear rocket engine test program
Calculational methods for nuclear rocket radiation shield design - radiation measurements in nuclear rocket propellant tank mockup using simulated liquid hydrogen
Calculational methods for nuclear rocket radiation shield design - analysis of radiation measurements in nuclear rocket propellant tank mockup using simulated liquid hydrogen
Nuclear rocket applications in Nuclear Flight Propulsion Module /NFPM/ and Reusable Nuclear Shuttle /RNS/
Nuclear rockets used for advanced propulsion systems
Nuclear rocket engine design for near-optimum vehicle performance for mission capability
Nuclear and explosive destruct concepts for nuclear rocket engines
Nuclear rocket applications, discussing performance, lunar logistics, solar system missions, orbital operations and payload data
Gaseous nuclear rocket technology studies for application to nuclear engines for rocket vehicles
Kiwi B nuclear rocket acoustics - sound pressure distribution, energy conversion, and power distribution
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.
Summary of nuclear reactors, fuels and operating principles of nuclear rockets
Specific nuclear light bulb and open-cycle vortex stabilized gaseous nuclear rocket engine designs
Nuclear rockets operating efficiency and flexibility, reliability, safety, hot high stress structures, nozzle cooling, etc