Publication Date:
2019-07-11
Description:
A two-body computerized mathematical model is used to calculate planar dynamics of the LADT #3 and supersonic BLDT parachute inflations. Results indicate that the calculated loads and motions of the LADT #3 inflation are not affected appreciably by variation in the suspension-line damping coefficient. However, variation of the coefficient results in significant changes in the calculated loads and strain rates of the supersonic BLDT inflation.
Keywords:
Spacecraft Design, Testing and Performance
Type:
LWP-1050
Format:
application/pdf
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