Add to ORKGVolume 1 presents a technical description of the Marshall Engineering Thermosphere (MET) model atmosphere and a summary of its historical development. Various programs developed to augment the original capability of the model are discussed in detail. The report also describes each of the individual subroutines developed to enhance the model. Computer codes for these subroutines are contained in four appendices
The separated flow method is evaluated. This method was developed for moderately swept wings with mu...
The Systems Autonomy Demonstration Project (SADP) produced a knowledge-based real-time control syste...
This volume contains the presentation charts of talks given at the "1997 Spacecraft Contamination an...
A computer model has been developed to simulate the processes involved in the operation of the Natio...
This Workshop on Stratospheric Models and Measurements (M&M) marks a significant expansion in the hi...
This Workshop on Stratospheric Models and Measurements (M&M) marks a significant expansion in the hi...
The Center for Space Construction (CSC) at the University of Colorado at Boulder is one of eight Uni...
The NASA Manned Spacecraft Center has been actively involved in the direction and support of program...
This paper describes a redesigned longitudinal controller that flew on the High-Alpha Research Vehic...
Advanced high performance vehicles, including Single-Stage-To-Orbit (SSTO) hypersonic flight vehicle...
The Office of Space Science and Applications (OSSA) is responsible for the overall planning, directi...
An investigation was made to determine the feasibility of using an aerobrake system for manned and u...
The design and development of an airborne flight-test experiment to study nonreacting gas jets injec...
Low-g accelerometers were used by NASA on a variety of flights for over 12 years. These flights have...
A concept for an orbiting laboratory for testing Controls-Structures Integration (CSI) technology is...
The separated flow method is evaluated. This method was developed for moderately swept wings with mu...
The Systems Autonomy Demonstration Project (SADP) produced a knowledge-based real-time control syste...
This volume contains the presentation charts of talks given at the "1997 Spacecraft Contamination an...
A computer model has been developed to simulate the processes involved in the operation of the Natio...
This Workshop on Stratospheric Models and Measurements (M&M) marks a significant expansion in the hi...
This Workshop on Stratospheric Models and Measurements (M&M) marks a significant expansion in the hi...
The Center for Space Construction (CSC) at the University of Colorado at Boulder is one of eight Uni...
The NASA Manned Spacecraft Center has been actively involved in the direction and support of program...
This paper describes a redesigned longitudinal controller that flew on the High-Alpha Research Vehic...
Advanced high performance vehicles, including Single-Stage-To-Orbit (SSTO) hypersonic flight vehicle...
The Office of Space Science and Applications (OSSA) is responsible for the overall planning, directi...
An investigation was made to determine the feasibility of using an aerobrake system for manned and u...
The design and development of an airborne flight-test experiment to study nonreacting gas jets injec...
Low-g accelerometers were used by NASA on a variety of flights for over 12 years. These flights have...
A concept for an orbiting laboratory for testing Controls-Structures Integration (CSI) technology is...
The separated flow method is evaluated. This method was developed for moderately swept wings with mu...
The Systems Autonomy Demonstration Project (SADP) produced a knowledge-based real-time control syste...
This volume contains the presentation charts of talks given at the "1997 Spacecraft Contamination an...