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I L SfS HK5M SMITHSONIAN ANNALS OF
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A Bibliographic Note The series Smi
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SMITHSONIAN ANNALS OF FLIGHT Throug
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VI SMITHSONIAN ANNALS OF FLIGHT 19.
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1 Some Jet Propulsion Formulas of O
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NUMBER 10 — — —— . . . -
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SMITHSONIAN ANNALS OF FLIGHT FIGURE
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During these years, in which the fu
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10 SMITHSONIAN ANNALS OF FLIGHT the
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12 SMITHSONIAN ANNALS OF FLIGHT FIG
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18 3. French Patent 318,667, 13 Feb
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20 SMITHSONIAN ANNALS OF FLIGHT tie
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Appendix Considerations Concerning
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NUMBER 10 In the present case, ther
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NUMBER 10 27 III Let us consider wh
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NUMBER 10 29 = 2100 sec, the rate w
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NUMBER 10 31 bring us far away from
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34 SMITHSONIAN ANNALS OF FLIGHT pro
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36 SMITHSONIAN ANNALS OF FLIGHT C \
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40 SMITHSONIAN ANNALS OF FLIGHT 0 1
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42 Figure 15. The dispersion of the
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44 SMITHSONIAN ANNALS OF FLIGHT sys
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46 SMITHSONIAN ANNALS OF FLIGHT com
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48 SMITHSONIAN ANNALS OF FLIGHT T,
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50 SMITHSONIAN ANNALS OF FLIGHT pla
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Robert H. Goddard and the Smithsoni
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NUMBER 10 to help Mr. Goddard in de
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NUMBER 10 61 flash powder which mig
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NUMBER 10 63 FIGURE 5.—Modificati
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NUMBER 10 65
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NUMBER 10 tion for a U.S. patent on
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NUMBER 10 69 70. Goddard to Abbot,
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72 SMITHSONIAN ANNALS OF FLIGHT lif
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Recollections of Early Biomedical M
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NUMBER 10 r FIGURE 2.—First biome
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FIGURE 4.—Presentation by Dr. Con
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Astrodynamics is defined in terms o
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NUMBER 10 83 But it should be recog
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NUMBER 10 85 were experimenting in
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Vladimir Mandl: Founding Writer on
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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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224 SMITHSONIAN ANNALS OF FLIGHT Al
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226 SMITHSONIAN ANNALS OF FLIGHT de
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228 SMITHSONIAN ANNALS OF FLIGHT Th
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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
Page 267: NUMBER 10 257 6. Small gyroscopic a
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Page 274 and 275: 264 B C FIGURE 7.—Drawing from Sw
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Page 279 and 280: 24 Some New Data on Early Work of t
Page 281 and 282: NUMBER 10 271 jy.. FIGURE 3. /# £
Page 283 and 284: NUMBER 10 273 conclusions, which we
Page 285 and 286: NUMBER 10 275 thrust engines. A for
Page 287 and 288: 25 Early Developments in Rocket and
Page 289 and 290: NUMBER 10 279 Time reference 5 sec
Page 291 and 292: NUMBER 10 281 During measurement of
Page 293 and 294: NUMBER 10 283 First Personal Involv
Page 295: NUMBER 10 285 on the Wasserkuppe, o
Page 298 and 299: 288 SMITHSONIAN ANNALS OF FLIGHT Ch
Page 305 and 306: 27 Annapolis Rocket Motor Developme
Page 307 and 308: NUMBER 10 297 I remember being so f
Page 309 and 310: NUMBER S P. (P»i) P, (psi) Po (psi
Page 311: NUMBER 10 301 Figure 6 shows these
Page 314 and 315: 304 Frank-Kamenetskiy, D.A., 193 Fr
Page 316 and 317: 306 SMITHSONIAN ANNALS OF FLIGHT Ro
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