Static stability and drag characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0

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035 ‡a(MiU)99187625998306381
035 ‡asdr-miu.99187625998306381
035 ‡a(OCoLC)1333449677
035 ‡a(GWLA)gwla on1333449677
040 ‡aTRAAL ‡beng ‡erda ‡cTRAAL
049 ‡aMAIN
086 0 ‡aD 301.45/33: 74-024
100 1 ‡aBest, J. T., ‡cJr., ‡eauthor,
245 1 0 ‡aStatic stability and drag characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0 / ‡cJ.T. Best, Jr. and R.W. Rhudy.
264 1 ‡aArnold Air Force Base, Tennessee : ‡bArnold Engineering Development Center, Air Force Systems Command, United States Air Force, ‡c1974.
300 ‡a94 pages : ‡billustrations, ‡c28 cm
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aAEDC-TR ; ‡v74-024
500 ‡aReport was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.
500 ‡a"Final Report for Period September 4 -- 13, 1973."
500 ‡a"April 1974."
504 ‡aIncludes bibliograqphic references (page 17).
520 ‡aStatic-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the High Altitude Supersonic Target (HAST) missile.
533 ‡aPhotocopy.
538 ‡aMode of access: Internet.
650 0 ‡aDrag (Aerodynamics)
650 0 ‡aGuided missiles ‡xAerodynamics.
650 0 ‡aGuided missiles ‡xTesting.
700 1 ‡aRhudy, R. W., ‡eauthor.
710 2 ‡aARO, Inc., ‡esponsor.
710 2 ‡aArnold Engineering Development Center, ‡esponsor.
710 1 ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015104953032
CID ‡a102892457
DAT 0 ‡a20220802101955.0 ‡b20241209000000.0
DAT 1 ‡a20241209061151.0 ‡b2024-12-09T14:45:35Z
DAT 2 ‡a2024-05-27T17:30:02Z
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