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