Two-thirds of the 149 papers presented were directly associated with space project applications of scientific, earth observation, and telecommunication satellites, reporting hardware design, development, and testing and related experiences of major space contractors. The other one-third covered important technological advances in satellite structural design, development and verification. As a result, the sessions were particularly useful to spacecraft mechanical engineers. (MM).
Spacecraft Structures and Mechanical Testing. Volume 1
1991
489 pages
Report
Keine Angabe
Englisch
Unmanned Spacecraft , Manned Spacecraft , Reentry vehicles , Spacecraft , Computer aided design , Composite materials , Aerodynamic characteristics , Telecommunications , Launchers , Fluid dynamics , Spacecraft trajectories , Acoustic properties , Reconnaissance satellites , Mathematical models , Computerized simulation , Orbits , Vibration , Symposia , Stress analysis , Debris , Netherlands , Polymers , Laminates , Finite element analysis , Structural analysis , Damage assessment , Fiber reinforced composites , Damping , Shock(Mechanics) , Matrix materials , Moisture content , Fracture(Mechanics) , Impact strength , Crack propagation , Structural response , Buckling , Space shuttles , Launching , Hydrodynamic codes , Gravity , Fatigue(Mechanics) , Heat shields , Beryllium , Trusses , Tolerances(Mechanics) , Design criteria , Micromechanics , Communication satellites , Space stations , Booster rocket engines , Reflectors , Delamination , Foreign technology , Foreign reports , Advanced composites , Microgravity , Impact loading , Vibroacoustics
Spacecraft Structures and Mechanical Testing, Volume 1
NTIS | 1991
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