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40 SMITHSONIAN ANNALS OF FLIGHT 0 10 20 30 centesimi di wcondo t FIGURE 10.—Comparative pressure records in closed chamber for cordite and C-powder. E IS us sir ft ZS 30 3S *0 IS T (.01 sec) FIGURE 11.—Pressure records (in atm vs. time in sec): a, C-powder combustion within test chamber shown in Figure 1; b, C-powder combustion within test chamber shown in Figure 5.
NUMBER 10 a QK 40 30 20 10 n* • Cordite austHaca o Polvere C - — i 100 200 - - - • i — — i —- — < -\ ! i r — - i j i i i n i •z r . -, - i i I i i • 1 —' i 1. i i i i ; i I 1 1 i y^\ V/^- i -- 1 • i p I. J i j ; i 1 i i ! 11 : ,_. ; 1 i ! ! I ! ! ' i i ! ; i Q-0,4p 0 - 75 11: 41 • : ! ; r -4 , 1 . 1 i ! ' ' • 1 i i 1 1 J 1 300 400 500 p atm. FIGURE 12.—Terminal pressure in closed chamber vs. charge weight for cordite and C-powder. -J-H-i FIGURE 13.—Test chamber for three tubular grains. x . • : ' i I . , i_..:, i 1 ! 1 i _ 1 !
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Page 4 and 5: A Bibliographic Note The series Smi
Page 6 and 7: SMITHSONIAN ANNALS OF FLIGHT Throug
Page 8 and 9: VI SMITHSONIAN ANNALS OF FLIGHT 19.
Page 11 and 12: 1 Some Jet Propulsion Formulas of O
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Page 16 and 17: SMITHSONIAN ANNALS OF FLIGHT FIGURE
Page 18 and 19: During these years, in which the fu
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Page 28 and 29: 18 3. French Patent 318,667, 13 Feb
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Page 33 and 34: Appendix Considerations Concerning
Page 35 and 36: NUMBER 10 In the present case, ther
Page 37 and 38: NUMBER 10 27 III Let us consider wh
Page 39 and 40: NUMBER 10 29 = 2100 sec, the rate w
Page 41: NUMBER 10 31 bring us far away from
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Page 52 and 53: 42 Figure 15. The dispersion of the
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Page 67 and 68: Robert H. Goddard and the Smithsoni
Page 69 and 70: NUMBER 10 to help Mr. Goddard in de
Page 71 and 72: NUMBER 10 61 flash powder which mig
Page 73 and 74: NUMBER 10 63 FIGURE 5.—Modificati
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Page 77 and 78: NUMBER 10 tion for a U.S. patent on
Page 79: NUMBER 10 69 70. Goddard to Abbot,
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Page 85 and 86: Recollections of Early Biomedical M
Page 87 and 88: NUMBER 10 r FIGURE 2.—First biome
Page 89 and 90: FIGURE 4.—Presentation by Dr. Con
Page 91 and 92: Astrodynamics is defined in terms o
Page 93 and 94: NUMBER 10 83 But it should be recog
Page 95 and 96: NUMBER 10 85 were experimenting in
Page 97 and 98: Vladimir Mandl: Founding Writer on
Page 99 and 100: NUMBER 10 89 PATENTNl OftAD REPUBLI
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10 Developments in Rocket Engineeri
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NUMBER 10 93 FIGURE 2.—The first
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NUMBER 10 FIGURE 4.—The ORM-9 eng
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NUMBER 10 97 FIGURE 9.—ORM-50 eng
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NUMBER 10 99 Section along AA Firin
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NUMBER 10 101 FIGURE 13.—The expe
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11 A Historical Review of Developme
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NUMBER 10 105 FIGURE 5.—Lithergol
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NUMBER 10 that the possibility of a
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NUMBER 10 109 the contrary; we then
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NUMBER 10 111 rocket combustion cha
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12 On the GALCIT Rocket Research Pr
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NUMBER 10 115 The undertaking we ha
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NUMBER 10 117 advise on the support
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NUMBER 10 methyl-alcohol rocket mot
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NUMBER 10 121 5. "Rocket Performanc
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NUMBER 10 123 FIGURE 5.—Overall v
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NUMBER 10 on the possibility of usi
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NUMBER 10 33. Letters (note 14). 34
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130 SMITHSONIAN ANNALS OF FLIGHT ce
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132 SMITHSONIAN ANNALS OF FLIGHT of
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134 SMITHSONIAN ANNALS OF FLIGHT A
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136 SMITHSONIAN ANNALS OF FLIGHT Re
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138 SMITHSONIAN ANNALS OF FLIGHT FI
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140 SMITHSONIAN ANNALS OF FLIGHT ca
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142 SMITHSONIAN ANNALS OF FLIGHT so
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144 SMITHSONIAN ANNALS OF FLIGHT 2
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146 SMITHSONIAN ANNALS OF FLIGHT St
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148 SMITHSONIAN ANNALS OF FLIGHT A-
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150 SMITHSONIAN ANNALS OF FLIGHT CH
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152 SMITHSONIAN ANNALS OF FLIGHT LI
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15 Ludvik OcenaSek: Czech Rocket Ex
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NUMBER 10 159 FIGURE 2.—Ludvik Oc
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NUMBER 10 161 FIGURE 5.—Ludvik Oc
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NUMBER 10 163 FICURE 6.—a, Launch
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NUMBER 10 165 quarry near Prague. E
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168 SMITHSONIAN ANNALS OF FLIGHT re
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170 SMITHSONIAN ANNALS OF FLIGHT I
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172 SMITHSONIAN ANNALS OF FLIGHT Th
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174 SMITHSONIAN ANNALS OF FLIGHT Ve
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17 First Rocket and Aircraft Flight
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NUMBER 10 179 The rocket project wa
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NUMBER 10 181 FIGURE 2.—Second st
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NUMBER 10 FIGURE 3.—DM-2 ramjet e
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18 On Some Work Done in Rocket Tech
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NUMBER 10 187 FICURE 3.—Launching
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NUMBER 10 189 on the smoked tape. A
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NUMBER 10 191 FIGURE 9.—Indicatin
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NUMBER 10 193 FIGURE 13.—Control
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NUMBER 10 195 2000 rpm by rotating
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NUMBER 10 197 Lubricant ^ 9a' " FIG
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NUMBER 10 199 of radio signals to t
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NUMBER 10 201 1. Register of experi
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204 SMITHSONIAN ANNALS OF FLIGHT te
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206 SMITHSONIAN ANNALS OF FLIGHT be
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208 SMITHSONIAN ANNALS OF FLIGHT 6.
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212 SMITHSONIAN ANNALS OF FLIGHT 3-
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A^ -/••••••.\ D+ VE •
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216 SMITHSONIAN ANNALS OF FLIGHT NO
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218 SMITHSONIAN ANNALS OF FLIGHT Vi
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222 SMITHSONIAN ANNALS OF FLIGHT Co
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230 SMITHSONIAN ANNALS OF FLIGHT wi
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232 SMITHSONIAN ANNALS OF FLIGHT th
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234 SMITHSONIAN ANNALS OF FLIGHT wa
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236 SMITHSONIAN ANNALS OF FLIGHT In
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238 SMITHSONIAN ANNALS OF FLIGHT ab
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240 diesel fuel and lox began on th
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242 14 May 1940: Reviewed layout fo
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248 SMITHSONIAN ANNALS OF FLIGHT th
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250 SMITHSONIAN ANNALS OF FLIGHT tl
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NUMBER 10 253 FIGURE 6.—a, Model
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NUMBER 10 255 FIGURE 9.—Winged ro
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NUMBER 10 257 6. Small gyroscopic a
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262 SMITHSONIAN ANNALS OF FLIGHT N?
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264 B C FIGURE 7.—Drawing from Sw
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266 SMITHSONIAN ANNALS OF FLIGHT in
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24 Some New Data on Early Work of t
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NUMBER 10 271 jy.. FIGURE 3. /# £
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NUMBER 10 273 conclusions, which we
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NUMBER 10 275 thrust engines. A for
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25 Early Developments in Rocket and
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NUMBER 10 279 Time reference 5 sec
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NUMBER 10 281 During measurement of
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NUMBER 10 283 First Personal Involv
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NUMBER 10 285 on the Wasserkuppe, o
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288 SMITHSONIAN ANNALS OF FLIGHT Ch
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27 Annapolis Rocket Motor Developme
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NUMBER 10 297 I remember being so f
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NUMBER S P. (P»i) P, (psi) Po (psi
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NUMBER 10 301 Figure 6 shows these
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304 Frank-Kamenetskiy, D.A., 193 Fr
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306 SMITHSONIAN ANNALS OF FLIGHT Ro
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TUT10N NOIifUIISNt NVINOSHlitNS S3f
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