Abstract
Attention is called to the importance of including the roles of cosmic dust particles and rocket exhaust particles in the detailed analysis of spacecraft charging effects, arcing and power drains due to leakage currents. Aspects of the problem pertaining to both low and high (geosynchronous) Earth orbit are discussed. Recommendations are made to assessing the long-term effects of hypervelocity impacts of these particles.
Full Text 
Sign-in/Register to access full text options
Sign-in/Register to access full text options 
Paper version not known
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
