The orbital debris environment model contained in this report is intended to be used by the spacecraft community for the design and operation of spacecraft in low Earth orbit. This environment, when combined with material dependent impact tests and spacecraft failure analysis, is intended to be used to evaluate spacecraft vulnerability, reliability, and shielding requirements. The environment represents a compromise between existing data to measure the environment, modeling of these data to predict the future environment, the uncertainty in both measurements and modeling, and the need to describe the environment so that various options concerning spacecraft design and operations can be easily evaluated.
Orbital Debris Environment for Spacecraft Designed to Operate in Low Earth Orbit
1989
23 pages
Report
No indication
English
Unmanned Spacecraft , Manned Spacecraft , Space Safety , Spacecraft , Debris , Low orbit trajectories , Requirements , Measurement , Uncertainty , Space environments , Earth orbits , Hazards , Impact tests , Vulnerability , Test methods , Reliability , Shielding , Collisions , Risk analysis , BMDO(Ballistic Missile Defense Organization)