- Page 2 and 3:
Spink, Barry L Civ USAF AETC AFHRAJ
- Page 4 and 5:
, , ·::'i~,:~~'rg~~' DECLASSIFIED
- Page 6 and 7:
AUT H 0 R I Z A T ION ThiS ~terial
- Page 8 and 9:
of prototype and ne;'1 production e
- Page 10 and 11:
• • Co s t of OpeLa tlon ~ 1952
- Page 12 and 13:
- APPENprCES: A Sununary of AFF'X A
- Page 14 and 15:
(I 11 Charts: Page Cor:1.manders to
- Page 16 and 17:
" -, :- SUPPGE'rIHG 'l'Ar:, Hq A..
- Page 18 and 19:
Fag.:: r I 8 Dec 1949 I.: Feb 1951
- Page 20 and 21:
Page 26 Hay 1958 1 Jul 1958 17 Oc t
- Page 22 and 23:
t ·~ ~~ .jor· y,obert 11 . Io/hit
- Page 24 and 25:
1 Ghapter 1 HIS'roRY OF ASSIGHED UJ
- Page 26 and 27:
3 The XP-81 and xp-84 arr1ved at Mu
- Page 28 and 29:
5 Wing crashed during a test f11ght
- Page 30 and 31:
7 defunct 2159th Experimental Wing,
- Page 32 and 33:
9 Approval of the tofaster Plan si
- Page 34 and 35:
I 11 Mea.nwhlle, units were moving
- Page 36 and 37:
13 the 6S15th Armanent and Elec tro
- Page 38 and 39:
Growth and expansion affected Cente
- Page 40 and 41:
17 General Cooper was assigned to
- Page 42 and 43:
J In SU Dl i .t s hould be noted t
- Page 44 and 45:
23. 6510th USAF Hospital 'flas disc
- Page 46 and 47:
~TU:18 for Ell1..--:gto n AFH IlIhe
- Page 48 and 49:
- lie'"" ........ 1I"".a.. F::R~E F
- Page 50 and 51:
ltetircr.lents '{a.s,ter ::;'C!':t'
- Page 52 and 53:
.'.. education.al asnlgnment and re
- Page 54 and 55:
Aircraft Inventor; Ninety-one aircr
- Page 56 and 57:
Branch inspection of all other J79-
- Page 58 and 59:
and development of the Qyna-Soar f1
- Page 60 and 61:
I ~ . Also, the AF?TC D1rec tora te
- Page 62 and 63:
I on vehicles undergoing flight tes
- Page 64 and 65:
40 An Aerospace Research Pilot Cour
- Page 66 and 67:
I : { Funds \....ere denied f'or de
- Page 68 and 69:
filS?? a 44 Chapter 3 THE AIR FORCE
- Page 70 and 71:
:1 wFiiil 46 U co~~erc1al jet aircr
- Page 72 and 73:
§ E jJ £ , line rB.iIlge southwar
- Page 74 and 75:
Z'E 5 £ Ie 50 practice rendezvous
- Page 76 and 77: I 52 Solid Rocket captive Test Fa,
- Page 78 and 79: ;;.iJ ,..I • support of industry"
- Page 80 and 81: unt1l 1 February 1958 "then he ',':
- Page 82 and 83: In mid-Apr'11 19S3~ the Aer'ojet Ge
- Page 84 and 85: 60 2.no. Oc toher 1957 J 0 ver $40,
- Page 86 and 87: 62 Brigadier General ~~rc~s F, Coop
- Page 88 and 89: ," I , Q q . pr'opulslo!l developme
- Page 90 and 91: Directs the research and developmen
- Page 92 and 93: olaf & RET F 68 launch from a tube
- Page 94 and 95: 70 the nurnber of personnel as dep1
- Page 96 and 97: ... \ . ' 1,-1 engine f1 'r1 n g~ o
- Page 98 and 99: , ' . 1.
- Page 100 and 101: ATLAS testing but was undergoing mo
- Page 102 and 103: f'S Direc torate 15 Instrumentation
- Page 104 and 105: :' I I I'; Chapter 5 DIRECTORATE OF
- Page 106 and 107: I ~ lc l\l d.e c d ~T'al d(:par·t~
- Page 108 and 109: 80 Directorate of F11ght Test and f
- Page 110 and 111: ',':ere conducted by other AFSC tes
- Page 114 and 115: 85 to control and monitor missile
- Page 116 and 117: Becauce of the hazc.rdou~ n 'l turc
- Page 118 and 119: \ t I f I '1 .. '. . : Close-up o
- Page 120 and 121: ·.. ; ., Dev~loprnent \
- Page 122 and 123: 91 of the modified airplane to 80 p
- Page 124 and 125: at high altitudes. Teet results als
- Page 128 and 129: Dur.ing an inverted spin, recovery
- Page 130 and 131: • Norai.r bLa.l t T-38 Talon traI
- Page 132 and 133: , 9 max1lnu:n speed was in the low
- Page 134: 101 ·,·:,e.t't.' USAF SiN 58-1192
- Page 137 and 138: 103 external fittings and ins talt
- Page 139 and 140: Although thE: test wa.s exceptional
- Page 141 and 142: lOi' test items. E."1g1ne SiN E230-
- Page 143 and 144: 109 hours. The f1rst flight was per
- Page 145 and 146: llJ. (grass, dustJ \·;ater J and s
- Page 147 and 148: 113 helicopter s ever tested by the
- Page 149 and 150: I guarantees, E1ghteen flights \'ie
- Page 151 and 152: 117 'The l~rre5tingGable Purpose o
- Page 153 and 154: p ~.__ ~ - • " , 119 compal'
- Page 155 and 156: 121 Bell, Douglas, North Amer1can,
- Page 157 and 158: I j 'I 123 eq1Jlpped with dual XLR-
- Page 159 and 160: 125 characteristics. EAch fl1ght by
- Page 161 and 162: 1'2(' , NHSA(AF/Navy X~l~ F11~,ts ,
- Page 163 and 164: 129 n~w ma.x1Il1).l11l speed of 3..
- Page 165 and 166: any portion of the X-15 ceckp1t :"
- Page 167 and 168: .. · .. In 1958, four huge engi
- Page 169 and 170: , ~ , .. ' stand (PSTS) rocket engi
- Page 171: Thirteen propulsion system t.est st