Meteoroid environment model, 1970 - Interplanetary and planetary. NASA space vehicle design criteria /environment/
Astronomical meteoroid environment model for space missions
SEARCH · Engineering Papers
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Astronomical meteoroid environment model for space missions
Application of human factors engineering to spacecraft habitability
Optimization design methods for spacecraft structural systems and subsystems
Internal loads and stresses caused by space vehicle vibration resulting from induced or natural environments
Aeroelastic spacecraft design to minimize buffeting during atmospheric ascent
Prelaunch, launch, and inflight earth orbital environment data for HEAO spacecraft
Analysis of transient loads produced by ignition of rocket engine during launch and flight operations for solid and liquid propellant rocket engines
Radiation torque sources and effects on spacecraft and spacecraft attitude control system design
Effects of nuclear and space radiation on mechanical, thermal, and optical properties of spacecraft structural materials
Meteoroid damage determination and spacecraft structure protection and reliability
Assessment of disturbance torques due to interaction of spacecraft with atmosphere in long duration orbits for use in design of spacecraft attitude control systems
Boundary layer transition thermodynamic test data for space shuttle configuration and trajectory analyses
Preventive maintenance instructions for bonding and electrical grounding systems to prevent equipment damage by electrical faults, lightning, and radiation - Vol. 3
Bearing requirements for liquid rocket engine turbopumps
Analysis of internal and external gas venting system of spacecraft
Analysis of loads produced on spacecraft by staging operations and practices to insure that staging loads are included in spacecraft design
Qualification tests conducted on flight quality components, subsystems, and systems to prove that structural design requirements have been achieved
Design approach for solid propellant rocket igniters