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Flugmechanik
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X B-70 Flight Test Data Comparisons with Simulation Predictions of Inlet Unstart and Buzz
Transonic Unsteady Aerodynamics for Planar Wings with Trailing Edge Control Surfaces
Transformations Applicable to Missile and Satellite Trajectory Computations
Towards Complete Configurations Using an Embedded Grid Approach
TOPEX/POSEIDON Operational Orbit Determination Results Using Global Positioning Satellites
Tilt-Rotor or Helicopter. An Evaluation of the Way Ahead for Marine Corps Medium-Lift Aviation
Three Dimensional Lightning Launch Commit Criteria Visualization Tool
The Station '' Zond-6'' Landed - Space ''Soundings'' Continued
The Optimization of Multi-Stage Orbit Transfer Processes by Dynamic Programming
The Effect of Separations at the Leading Edge on the Aerodynamic Features of Wings
Test Program for Stirling Radioisotope Generator Hardware at NASA Glenn Research Center
Techniques for the Analysis of Spectral and Orbital Congestion in Space Systems
Switch Program Documentation Interim Report, 8 Mar. 1969 - 8 Mar. 1970
Subroutine Descriptions and Listings for the Orbit Determination Program, Volume 2 Final Report
Subroutine Descriptions and Listings for the Orbit Determination Program, Volume 1 Final Report
Study of Low-Acceleration Space Transportation Systems Summary Report, Jul. 1964 - Jun. 1965
Static Lift Characteristics of Jet Slots: A Clarifying Study of the External Ejector
Space Station Systems Analysis Study. Part 2, Volume 2
Space Shuttle Aerodynamic Characteristics of the Nr delta Wing Orbiter, M Equals 0.6 to 1.3
Space Shuttle Abort Separation Pressure Investigation. Volume 6 Orbiter Data at Mach 2
Space Shuttle Abort Separation Pressure Investigation. Volume 5 Booster Data at Mach 2
Space Shuttle Abort Separation Pressure Investigation. Volume 4 Orbiter Data at Mach 3
Space Shuttle Abort Separation Pressure Investigation. Volume 3 Booster Data at Mach 3
Space Shuttle Abort Separation Pressure Investigation. Volume 2, Part B Orbiter Data at Mach 5
Space Shuttle Abort Separation Pressure Investigation. Volume 1, Part B Booster Data at Mach 5