NASA NTRS · 19790022073
Pilot cryo tunnel: Attachments, seals, and insulation
Abstract
Several different tests are described which simulated the actual configuration of a cryogenic wind tunnel operating at pressures up to 5 atmospheres (507 kPa) and temperatures from -320 F (78K) to 120 F (322K) in order to determine compatible bolting, adequate sealing, and effective insulating materials. The evaluation of flange attachments (continuous threaded studs) considered bolting based on compatible flanges, attachment materials, and prescribed bolt elongations. Various types of seals and seal configurations were studied to determine suitability and reusability under the imposed pressure and temperature loadings. The temperature profile was established for several materials used for structural supports.
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Wilson, J. F., Ware, G. D., Ramsey, J. W., Jr.. 1974-01-01. Pilot cryo tunnel: Attachments, seals, and insulation. https://ntrs.nasa.gov/citations/19790022073
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