Add to ORKGThe topics are presented in viewgraph form and include the following: total engine system management critical to successful nuclear thermal rocket engine (NTRE) start up; NERVA type engine start windows; reactor power control; heterogeneous reactor cooling; propellant feed system dynamics; integrated NTRE start sequence; moderator cooling loop and efficient NTRE starting; analytical simulation and low risk engine development; accurate simulation through dynamic coupling of physical processes; and integrated NTRE and mission performance
A critical enabling technology in the evolutionary development of nuclear thermal propulsion (NTP) i...
NTR: High thrust high specific impulse (2 x LOXLH2 chemical) engine uses high power density fission ...
The Nuclear Thermal Rocket Element Environmental Simulator (NTREES) facility is designed to perform ...
The topics are presented in viewgraph form and include the following: systems approach needed for nu...
The topics are presented in viewgraph form and include the following: nuclear thermal rocket (NTR) m...
Results of a feasibility analysis of a long life, reusable nuclear thermal rocket engine are present...
Four Revised Point of Departure NTR Engines were Designed and Analyzed using MCNP and NESS. All Four...
A demonstration of a Nuclear Thermal Propulsion (NTP) engine has not been conducted in over 50 years...
A key technology element in Nuclear Thermal Propulsion is the development of fuel materials and comp...
A preferred Pratt & Whitney conceptual Nuclear Thermal Rocket Engine (NTRE) has been designed based ...
In FY11, NASA formulated a plan for Nuclear Thermal Propulsion (NTP) development that included Found...
Four nuclear thermal rocket (NTR) models have been created in the Numerical Propulsion System Simula...
Nuclear Thermal Propulsion (NTP) is a concept which uses a nuclear reactor to heat a propellant to h...
Nuclear thermal propulsion has long been considered an enabling technology for human missions to Mar...
In FY'11, Nuclear Thermal Propulsion (NTP) was identified as a key propulsion option under the Advan...
A critical enabling technology in the evolutionary development of nuclear thermal propulsion (NTP) i...
NTR: High thrust high specific impulse (2 x LOXLH2 chemical) engine uses high power density fission ...
The Nuclear Thermal Rocket Element Environmental Simulator (NTREES) facility is designed to perform ...
The topics are presented in viewgraph form and include the following: systems approach needed for nu...
The topics are presented in viewgraph form and include the following: nuclear thermal rocket (NTR) m...
Results of a feasibility analysis of a long life, reusable nuclear thermal rocket engine are present...
Four Revised Point of Departure NTR Engines were Designed and Analyzed using MCNP and NESS. All Four...
A demonstration of a Nuclear Thermal Propulsion (NTP) engine has not been conducted in over 50 years...
A key technology element in Nuclear Thermal Propulsion is the development of fuel materials and comp...
A preferred Pratt & Whitney conceptual Nuclear Thermal Rocket Engine (NTRE) has been designed based ...
In FY11, NASA formulated a plan for Nuclear Thermal Propulsion (NTP) development that included Found...
Four nuclear thermal rocket (NTR) models have been created in the Numerical Propulsion System Simula...
Nuclear Thermal Propulsion (NTP) is a concept which uses a nuclear reactor to heat a propellant to h...
Nuclear thermal propulsion has long been considered an enabling technology for human missions to Mar...
In FY'11, Nuclear Thermal Propulsion (NTP) was identified as a key propulsion option under the Advan...
A critical enabling technology in the evolutionary development of nuclear thermal propulsion (NTP) i...
NTR: High thrust high specific impulse (2 x LOXLH2 chemical) engine uses high power density fission ...
The Nuclear Thermal Rocket Element Environmental Simulator (NTREES) facility is designed to perform ...