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98 SMITHSONIAN ANNALS OF FLIGHT Total Section along EF Section along CD Wrapped in tin & soldered all around View along arrow A To manometer Oxidizer FIGURE 10.—The ORM-52 engine was designed in 1933 and passed static acceptance tests in that year. Designated for experimental rockets and naval torpedoes, it used nitric acid and kerosene as propellants. Engine data were as follows: Thrust at ground level 250-310 kg; specific thrust 210 sec; chamber pressure 20-25 atm; excess oxidant ratio 1.08; fuel feed pressure 40 atm; ignition, hypergolic; combustion chamber volume 2.25 1; engine weight 14.5 kg.
NUMBER 10 99 Section along AA Firing ca Electric primer, spark plug current receiv igniting compound shunt Total length 465 Certificate to liquid fuel _. rocket engine ORM-65, No. 1 Fuel i nta ke B—MBaar"""'""! liretnopT^ Qxj_d_izer intake — w—IWIM. (mi ""• nAcnopT „. qPfi-ti
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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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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
Page 75 and 76: NUMBER 10 65
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
Page 101 and 102: 10 Developments in Rocket Engineeri
Page 103 and 104: NUMBER 10 93 FIGURE 2.—The first
Page 105 and 106: NUMBER 10 FIGURE 4.—The ORM-9 eng
Page 107: NUMBER 10 97 FIGURE 9.—ORM-50 eng
Page 111 and 112: NUMBER 10 101 FIGURE 13.—The expe
Page 113 and 114: 11 A Historical Review of Developme
Page 115 and 116: NUMBER 10 105 FIGURE 5.—Lithergol
Page 117 and 118: NUMBER 10 that the possibility of a
Page 119 and 120: NUMBER 10 109 the contrary; we then
Page 121 and 122: NUMBER 10 111 rocket combustion cha
Page 123 and 124: 12 On the GALCIT Rocket Research Pr
Page 125 and 126: NUMBER 10 115 The undertaking we ha
Page 127 and 128: NUMBER 10 117 advise on the support
Page 129 and 130: NUMBER 10 methyl-alcohol rocket mot
Page 131 and 132: NUMBER 10 121 5. "Rocket Performanc
Page 133 and 134: NUMBER 10 123 FIGURE 5.—Overall v
Page 135 and 136: NUMBER 10 on the possibility of usi
Page 137: NUMBER 10 33. Letters (note 14). 34
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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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154 SMITHSONIAN ANNALS OF FLIGHT FI
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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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220 SMITHSONIAN ANNALS OF FLIGHT 19
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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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246 SMITHSONIAN ANNALS OF FLIGHT 26
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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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