Method for verifying stable lunar surface takeoff of spacecraft
A technology for verifiers and spacecraft, applied in the testing of machines/structural components, simulators of space navigation conditions, instruments, etc., can solve problems such as uncertain take-off attitudes, differences in gravity environments, new missions, etc., to improve safety , High safety, ensure safety effect
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[0077] Step 1. According to the ground thrust reduction coefficient k of the orbital control engine of the spacecraft taking off from the lunar surface, the mass M a , the dry weight (weight without propellant) of the take-off demonstrator is designed as (kM a -M t ), where M t For the propellant filling amount of the take-off verifier, the moment of inertia and the position of the center of mass need to be set to be consistent with those of the lunar surface take-off spacecraft, where the error of the moment of inertia is less than 10%, the position deviation of the lateral center of mass is ≤2mm, and the deviation of the longitudinal center of mass is ≤5mm;
[0078] Step 2. Complete the propellant filling of the take-off verifier, the filling amount M t , to complete the quality characteristic test and the center of mass balance;
[0079] Step 3. Identify and calculate the disturbance moment experienced by the verifier in the ground test, and integrated value of lunar s...
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