Considerations of turbine cooling systems for Mach 3 flight

LDR 01304cam a2200349Ia 4500
001 011442378
003 MiAaHDL
005 20141009010000.0
006 m d
007 cr bn ---auaua
008 070403s1968 dcua b f000 0 eng d
019 ‡a86067700
035 ‡asdr-uiuc6395527
035 ‡a(OCoLC)122262880
040 ‡aAD# ‡cAD# ‡dEGM ‡dSZT
041 0 ‡aeng
049 ‡aUIUU
082 ‡a629.134353 ‡220
086 0 ‡aNAS 1.14:D-4491
088 ‡aNASA-TN-D-4491
100 1 ‡aStepka, Francis S.
245 1 0 ‡aConsiderations of turbine cooling systems for Mach 3 flight / ‡cFrancis S. Stepka.
246 3 ‡aNASA TN D-4491
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡aSpringfield, VA : ‡bFor sale by the Clearinghouse for Federal Scientific and Technical Information, ‡c1968.
300 ‡a41 p. : ‡bill. ; ‡c26 cm.
490 0 ‡aNASA technical note ; ‡vD-4491
500 ‡aCover title.
500 ‡a"April 1968."
504 ‡aIncludes bibliographical references (p. 32).
538 ‡aMode of access: Internet.
650 0 ‡aAerofoils ‡xMotors ‡xCooling systems.
650 0 ‡aAerofoils ‡xCooling ‡xMethodology.
650 0 ‡aAerofoils ‡xCooling ‡xDesign and construction.
710 2 ‡aLewis Research Center.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ‡a011442378
DAT 0 ‡a20101104153255.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2025-01-02T19:13:47Z
DAT 2 ‡a2025-01-02T18:30:02Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ‡aBK
HOL ‡0sdr-uiuc6395527 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106914721 ‡sUIU ‡16395527
974 ‡bUIU ‡cUIUC ‡d20250102 ‡sgoogle ‡uuiug.30112106914721 ‡y1968 ‡rpd ‡qbib ‡tUS fed doc