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Statistical analysis of landing contact conditions for three lifting body research vehiclesThe landing contact conditions for the HL-10, M2-F2/F3, and the X-24A lifting body vehicles are analyzed statistically for 81 landings. The landing contact parameters analyzed are true airspeed, peak normal acceleration at the center of gravity, roll angle, and roll velocity. Ground measurement parameters analyzed are lateral and longitudinal distance from intended touchdown, lateral distance from touchdown to full stop, and rollout distance. The results are presented in the form of histograms for frequency distributions and cumulative frequency distribution probability curves with a Pearson Type 3 curve fit for extrapolation purposes.
Document ID
19720011245
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Larson, R. R.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1972
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-6708
H-684
Report Number: NASA-TN-D-6708
Report Number: H-684
Accession Number
72N18895
Funding Number(s)
PROJECT: RTOP 727-01-01-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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