Static force and moment test of the Holloman narrow-gage rocket slet at Mach numbers from 3.5 to 5.5

LDR 01531nam a2200397Ii 4500
001 102893260
003 MiAaHDL
005 20241208000000.0
006 m d
007 cr bn ---auaua
008 220307s1987 tnua rbt f000 0 eng d
035 ‡a(MiU)99187625452506381
035 ‡asdr-miu.99187625452506381
035 ‡a(OCoLC)1302206763
035 ‡a(GWLA)gwla on1302206763
040 ‡aTRAAL ‡beng ‡erda ‡cTRAAL
049 ‡aMAIN
086 0 ‡aD 301.45/33: 87-V20
100 1 ‡aRatliff, C. L., ‡eauthor.
245 1 0 ‡aStatic force and moment test of the Holloman narrow-gage rocket slet at Mach numbers from 3.5 to 5.5 / ‡cC. L. Ratliff.
264 1 ‡aArnold Air Force Base, Tennessee : ‡bArnold Engineering Development Center, Air Force Systems Command, United States Air Force, ‡c1987.
300 ‡a45 pages : ‡billustrations, figures, tables ; ‡c28 cm
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aAEDC-TR ; ‡v87-V20
500 ‡a"Program Element 921A71."
500 ‡a"Final Report for period May 4-May 7, 1987."
500 ‡a"September 1987."
504 ‡aIncludes bibliographical references (page 9).
533 ‡aPrint reproduction.
538 ‡aMode of access: Internet.
650 0 ‡aMach number.
650 0 ‡aWind tunnel testing.
710 2 ‡aCalspan Corporation, ‡esponsor.
710 1 ‡aArnold Engineering Development Center, ‡eissuing body.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015104957033
CID ‡a102893260
DAT 0 ‡a20220802102027.0 ‡b20241208000000.0
DAT 1 ‡a20241208060856.0 ‡b2024-12-08T14:15:46Z
DAT 2 ‡a2024-08-07T17:30:02Z
CAT ‡aSDR-MIU ‡cmiu ‡dALMA ‡lprepare.pl-004-008
FMT ‡aBK
HOL ‡0sdr-miu.99187625452506381 ‡aMiU ‡bSDR ‡cGWLA ‡pmdp.39015104957033 ‡sMIU ‡199187625452506381
974 ‡bMIU ‡cGWLA ‡d20241208 ‡sgoogle ‡umdp.39015104957033 ‡y1987 ‡rpd ‡qbib ‡tUS fed doc