Solar electric propulsion application to Halley Comet flythrough and rendezvous missions, describing trajectory characteristics and payload capabilities
Halley's Comet flythrough and rendezvous missions via solar electric propulsion
ASTRODYNAMICS SPECIALISTS CONFERENCE ; 1971 ; FT. LAUDERDALE, FL, US
01.08.1971
Aufsatz (Konferenz)
Keine Angabe
Englisch