Aerodynamic characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0

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040 ⊔ ⊔ ‡aTRAAL ‡beng ‡erda ‡cTRAAL
049 ⊔ ⊔ ‡aMAIN
086 0 ⊔ ‡aD 301.45/33:72-006
100 1 ⊔ ‡aJones, J. H., ‡eauthor,
245 1 0 ‡aAerodynamic characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0 / ‡cJ.H. Jones.
264 ⊔ 1 ‡aArnold Air Force Base, Tennessee : ‡bArnold Engineering Development Center, Air Force Systems Command, United States Air Force, ‡c1972.
300 ⊔ ⊔ ‡a108 pages : ‡billustrations, ‡c28 cm
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
337 ⊔ ⊔ ‡aunmediated ‡bn ‡2rdamedia
338 ⊔ ⊔ ‡avolume ‡bnc ‡2rdacarrier
490 0 ⊔ ‡aAEDC-TR ; ‡v72-006
500 ⊔ ⊔ ‡aReport was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.
500 ⊔ ⊔ ‡a"Final Report: July 29 and 30, 1971."
500 ⊔ ⊔ ‡a"January 1972.."
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 Beech 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.
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 ⊔ ⊔ ‡a39015104952646
CID ⊔ ⊔ ‡a102892836
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DAT 1 ⊔ ‡a20241208060856.0 ‡b2024-12-08T14:15:12Z
DAT 2 ⊔ ‡a2024-07-29T17:30:02Z
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