Search
Now showing items 1-1 of 1
Optimal Low-Thrust Transfers to Lunar L1 Halo Orbit Using Variable Specific Impulse Engine
Publisher: American Society of Civil Engineers
Abstract: Given the advantages of variable specific impulse (VSI) engine, it is very likely that in the future there will be deep space missions that use this thrust as propulsion system. In this study, a design technique for a fuel ...
CSV
RIS