The topics are presented in viewgraph form and include the following: systems approach needed for nuclear thermal rocket (NTR) design optimization; generic NTR engine power balance codes; rocketdyne nuclear thermal system code; software capabilities; steady state model; NTR engine optimizer code-logic; reactor power calculation logic; sample multi-component configuration; NTR design code output; generic NTR code at Rocketdyne; Rocketdyne NTR model; and nuclear thermal rocket modeling directions
Results of a feasibility analysis of a long life, reusable nuclear thermal rocket engine are present...
In an effort to further refine potential point of departure nuclear thermal rocket engine designs, f...
A demonstration of a Nuclear Thermal Propulsion (NTP) engine has not been conducted in over 50 years...
Four nuclear thermal rocket (NTR) models have been created in the Numerical Propulsion System Simula...
The topics are presented in viewgraph form and include the following: nuclear thermal rocket (NTR) m...
The topics are presented in viewgraph form and include the following: total engine system management...
Four nuclear thermal rocket (NTR) models have been created in the Numerical Propulsion System Simula...
Viewgraphs on Enabler 1 and 2 engine system design modeling and comparisons are presented. The objec...
A critical enabling technology in the evolutionary development of nuclear thermal propulsion (NTP) i...
The topics are presented in viewgraph form and include the following: rocket engine transient simula...
The topics are presented in viewgraph form and include the following; nuclear thermal propulsion (NT...
The Rover/NERVA engine system is to be used as a reference, against which each of the other concepts...
The Nuclear Thermal Rocket (NTR) concept is being evaluated as a potential propulsion technology for...
Four Revised Point of Departure NTR Engines were Designed and Analyzed using MCNP and NESS. All Four...
The topics are presented in viewgraph form and include the following: nuclear thermal propulsion (NT...
Results of a feasibility analysis of a long life, reusable nuclear thermal rocket engine are present...
In an effort to further refine potential point of departure nuclear thermal rocket engine designs, f...
A demonstration of a Nuclear Thermal Propulsion (NTP) engine has not been conducted in over 50 years...
Four nuclear thermal rocket (NTR) models have been created in the Numerical Propulsion System Simula...
The topics are presented in viewgraph form and include the following: nuclear thermal rocket (NTR) m...
The topics are presented in viewgraph form and include the following: total engine system management...
Four nuclear thermal rocket (NTR) models have been created in the Numerical Propulsion System Simula...
Viewgraphs on Enabler 1 and 2 engine system design modeling and comparisons are presented. The objec...
A critical enabling technology in the evolutionary development of nuclear thermal propulsion (NTP) i...
The topics are presented in viewgraph form and include the following: rocket engine transient simula...
The topics are presented in viewgraph form and include the following; nuclear thermal propulsion (NT...
The Rover/NERVA engine system is to be used as a reference, against which each of the other concepts...
The Nuclear Thermal Rocket (NTR) concept is being evaluated as a potential propulsion technology for...
Four Revised Point of Departure NTR Engines were Designed and Analyzed using MCNP and NESS. All Four...
The topics are presented in viewgraph form and include the following: nuclear thermal propulsion (NT...
Results of a feasibility analysis of a long life, reusable nuclear thermal rocket engine are present...
In an effort to further refine potential point of departure nuclear thermal rocket engine designs, f...
A demonstration of a Nuclear Thermal Propulsion (NTP) engine has not been conducted in over 50 years...