On the Problem of Comet Orbit Determination for Spacecraft Intercept Missions
1967
89 pages
Report
Keine Angabe
Englisch
Spacecraft Trajectories & Flight Mechanics , Comet , Interception , Orbit calculation , Trajectory optimization , Algebra , Ascent , Calculation , Distance , Ephemeris , Error , Estimate , Linearity , Mission , Motion , Optimization , Orbit , Spacecraft , Trajectory
Ballistic intercept missions to Comet Encke
NTRS | 1975
|Ballistic Intercept Missions to Comet Encke
NTIS | 1975
|NTRS | 1963