01335cam a2200325Ia 4500011423777MiAaHDL20141013010000.0m d cr bn ---auaua920515s1992 dcua b f000 0 eng dsdr-uiuc6353965(OCoLC)25821594ABCABCLHLUIUUNAS 1.60:3145TL521.3.N18 no. 3145Thermal and structural tests of René 41 honeycomb integral-tank concept for future space transportation systems /John L. Shideler ... [et al.].Washington, D.C. :National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,1992.74 p. :ill. ;28 cm.NASA technical paper ;3145Prepared at Dryden Flight Research Facility.Includes bibliographical references (p. 13-14).Mode of access: Internet.High temperatures.Elasticity.Strains and stresses.Plates (Engineering)Testing.Space vehiclesMaterialsTesting.Honeycomb structuresMaterialsInfluence of temperature on.Honeycomb structuresMaterialsTesting.Shideler, John L.Dryden Flight Research Facility.01142377720100930134019.020141013010000.020141112173021.02025-01-02T19:02:41Z2025-01-02T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6353965uiugSDRUIUCuiug.30112106710566UIU6353965UIUUIUC20250102googleuiug.301121067105661992pdbibUS fed doc