NASA NTRS · 19820024435
Solid rocket booster sting interference wind tunnel test analysis, appendix D
Abstract
Additional analyses of wind tunnel test results from SRB sting interference test TWT 660 and HRWT 042 were conducted to evaluate the sting interference that may be present in the Space Shuttle SRB reentry aerodynamic math model. Additional wind tunnel data was obtained at higher angles of attack from test program TWT 660 and test program HRWT 042. The additional data were analyzed to evaluate the procedures used to fair the data in the development of the SRB reentry aerodynamic data Tape no. 5.
Keep this discovery
Explore connections, maps & timelines
Conine, B., Boyle, W.. 1982-08-01. Solid rocket booster sting interference wind tunnel test analysis, appendix D. https://ntrs.nasa.gov/citations/19820024435
Cite the original work for its findings. Save a collection to share your selection of sources.