Add to ORKGThe construction of detailed computational models of the dynamic behavior of various explosive ordnance devices used on space vehicles is discussed. The following topics are presented in viewgraph form: numerical methods, explosives and detonations, and the MESA computer code
This report presents the results of a series of wind tunnel tests showing the force, moment, and aut...
The results of tests to assess capacity loss in nickel hydrogen cells are presented in outline form....
Volume two of the facilities catalogue deals with Airbreathing Propulsion and Flight Simulation Faci...
Under a rotorcraft structural dynamics program sponsored by the NASA Langley Research Center, Sikors...
Autonomous Rendezvous and Docking (ARD) will be a requirement for future space programs. Clear examp...
This document consists of the presentation submitted at the Autonomous Rendezvous and Docking (ARD) ...
A ground vibration test was performed on the AH-64 (Apache) helicopter to determine the frequency re...
The viewgraphs and discussion of the ongoing activity at NASA Langley Research Center (LaRC) in supp...
Information on the Tethered Gravity Laboratory on the International Space Station is given in viewgr...
Analysis and design methods for laminated composite materials have been the subject of considerable ...
The focus is in the development of more accurate and efficient advanced methods for solution of sing...
Cello, piano. Duration: 22 minutes. At end: Wellesley, 9-6-51.https://repository.wellesley.edu/lamb/...
The main objective was to determine viable methods for starting the Space Shuttle Main Engine (SSME)...
Boeing Helicopters, together with other U.S. Helicopter manufacturers, is engaged in a finite elemen...
The issue of technology advancement and future space transportation vehicles is addressed. The chall...
This report presents the results of a series of wind tunnel tests showing the force, moment, and aut...
The results of tests to assess capacity loss in nickel hydrogen cells are presented in outline form....
Volume two of the facilities catalogue deals with Airbreathing Propulsion and Flight Simulation Faci...
Under a rotorcraft structural dynamics program sponsored by the NASA Langley Research Center, Sikors...
Autonomous Rendezvous and Docking (ARD) will be a requirement for future space programs. Clear examp...
This document consists of the presentation submitted at the Autonomous Rendezvous and Docking (ARD) ...
A ground vibration test was performed on the AH-64 (Apache) helicopter to determine the frequency re...
The viewgraphs and discussion of the ongoing activity at NASA Langley Research Center (LaRC) in supp...
Information on the Tethered Gravity Laboratory on the International Space Station is given in viewgr...
Analysis and design methods for laminated composite materials have been the subject of considerable ...
The focus is in the development of more accurate and efficient advanced methods for solution of sing...
Cello, piano. Duration: 22 minutes. At end: Wellesley, 9-6-51.https://repository.wellesley.edu/lamb/...
The main objective was to determine viable methods for starting the Space Shuttle Main Engine (SSME)...
Boeing Helicopters, together with other U.S. Helicopter manufacturers, is engaged in a finite elemen...
The issue of technology advancement and future space transportation vehicles is addressed. The chall...
This report presents the results of a series of wind tunnel tests showing the force, moment, and aut...
The results of tests to assess capacity loss in nickel hydrogen cells are presented in outline form....
Volume two of the facilities catalogue deals with Airbreathing Propulsion and Flight Simulation Faci...