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Stabilität
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keywords:(Stabilität)
Passive Isolation/Damping System for the Hubble Space Telescope Reaction Wheels
Exact Theory for the Stability of Caret Wings in Hypersonic Flow
Results of the Attitude Stabilisation of the ESRO-1 Satellite ( Aurorae)
Analysis of a Control System Containing Two Nonlinearities
Flight Results Obtained with a Non- Aerodynamic, Variable Stability, Flying Platform
Review of Propulsion-Induced Effects on Aerodynamics of Jet V/STOL Aircraft
Stability and Control CFD Investigations of a Generic 53 Degree Swept UCAV Configuration
A Dynamic Analysis of Aeroplanes Encountering Vortex Wake Turbulence
Wind-Tunnel Investigation of a 3/8-Scale Automobile Model over a Moving-Belt Ground Plane
The Effect of Lift on Entry Corridor Depth and Guidance Requirements for the Return Lunar Flight
Development of an Advanced Annular Combustor Final Report, 30 Jun. 1966 - 24 Apr. 1968
Aerothermodynamics of the Mars Global Surveyor Spacecraft
Stable White Coatings Interim Technical Progress Report, Jul. 3, 1964 - Mar. 2, 1965
Combustion Instability in Solid Propellant Rocket Motors Final Report
Inquiry on Container Top Safety. Second Edition. Updated until November 26, 1999
Unsteady Aerodynamic Analysis of Space Shuttle Vehicles. Part 3: Booster Interference Effects
Effects of Reynolds Number and Frequency Parameter on Control-Surface Buzz at High Subsonic Speeds
Application and Testing of Cuvertin 306, a Black Paint for Spacecraft Use
Wind-Tunnel Study of Deflected-Elevator Flutter Encountered on a T-Tail Airplane
Monte Carlo Approach to Touchdown Dynamics for Soft Lunar Landings
Experimental Study of Aeroelastic Instability of Overexpanded Rocket Nozzle Extensions
Tropical Climate Variability During the Satellite Era: What Can We Infer About Climate Sensitivity
Gyrometre Laser Triaxial Miniaturise (Miniaturized Triaxial Laser Gyro)
A Simulation of the Low Speed Handling of the Bac 221 Slender-Wing Research Aircraft
Study of a Soft Lander/Support Module for MARS Missions. Volume 1 - Summary Final Summary Report
Design, Development, and Utilization of General Purpose Airborne Simulator
Attitude Drift Analysis for the Wind and Polar Missions
Induced Rolling Moment Characteristics of the M557A Bomb at Mach Number 0.50 Streamline
Description and Performance of the Saturn Launch Vehicle's Navigation, Guidance, and Control System
Saturn 5, S-4 B Panel Flutter Qualification Test Final Report
Instability of the Rotor-Nacelle-Wing System Due to Aerodynamic Forces on Tilting-Rotor Aircraft
Selected Topics in Experimental Aeroelasticity at the NASA Langley Research Center