Electric propulsion spacecraft mission performance scaling laws for invariant trajectory, obtaining optimum gross payload over wide range of system input parameters
Performance scaling laws for electric propulsion mission analysis
AEROSPACE SCIENCES MEETING ; 1971 ; NEW YORK, NY
1971-01-01
Conference paper
No indication
English
Atmospheric Electric Propulsion Mission Performance Tool
Online Contents | 2014
|Atmospheric Electric Propulsion Mission Performance Tool
AIAA | 2014
|