3.3 Mission Analysis
67
Fig. 3.10 Relative position of 7500 N engine plume angle to laser 3D imaging sensor
Fig. 3.11 Stream line of
continuous flow of
throttlable engine plum at
1500 N when the distance to
lunar surface was 5 m
Fig. 3.12 Stream line of
continuous flow of
throttlable engine plum at
1500 N when the distance to
lunar surface was 3 m