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Title: Rockets, by Dr. Robert H. Goddard, Comprising "A method of reaching extreme altitudes" and "Liquid-propellant rocket development." With a new foreword by the author
Author: Robert Hutchings Goddard
Imprint: New York, [1946]


ID: 2-32-goddard
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Vol. I , Fig. 186. Bracing of Rocket
ID: SIL7-17-09
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Vol. I , Fig. 187. Poping System -- Upper Part
ID: SIL7-17-10
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Vol. I , Fig. 188. Bracing of Rocket
ID: SIL7-17-11
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Vol. I , Fig. 191. Bracing of Rocket -- January, 1927
ID: SIL7-17-12
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Vol. I , Fig. 214. Turn-table and Rocket
ID: SIL7-17-13
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Vol. I Fig. 217. Rocket Ready for Test, April 20, 1927
ID: SIL7-17-14
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Vol. I, Fig. 218. Rocket Ready for Test
ID: SIL7-17-15
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Vol. I , Fig. 233. Jacket on Combustion Chamber
ID: SIL7-17-16
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Vol. I , Fig. 239. Modified Supporting Lugs and Flanges
ID: SIL7-17-17
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Vol. I , Fig. 240. Completed Rocket -- July 20, 1927
ID: SIL7-17-18
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Vol. I , Fig. 241. Completed Rocket
ID: SIL7-17-19
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Vol. I , Fig. 245. Alcohol Stove on Combustion Chamber
ID: SIL7-17-20
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Vol. I , Fig. 246. Combustion Chamber
ID: SIL7-17-21
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Vol. I , Fig. 249. Complted Rocket - August 31, 1927
ID: SIL7-17-22
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Vol. I , Fig. 250. Completed Rocket
ID: SIL7-17-23
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Vol. III , Fig. 3. Oxygen and Gasoline Orifices, Dent Type
ID: SIL7-17-24
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Vol. III , Fig. 4. Oxygen and Gasoline Orifices, Dent Type
ID: SIL7-17-25
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Vol. III , Fig. 20. Injection Head of Chamber Used in Second Test of March 4, 1930
ID: SIL7-17-26
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Vol. IV , Fig. 7. Rocket. Used in Tests Nos. 71 and 72
ID: SIL7-17-27
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Vol. XI , Fig. 31. Tower and Rocket
ID: SIL7-17-28
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Vol. XI , Fig. 32. Rocket in Tower
ID: SIL7-17-29
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Vol. XI , Fig. 40. Set-up for Testof Augst 9, 1938
ID: SIL7-17-30
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Vol. XI , Fig. 41. Rocket in Flight
ID: SIL7-17-31
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Vol. XI , Fig. 44. Committee Holding Parachute
ID: SIL7-17-32
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Vol. I, Fig. 145. Tapered Nozzle as Flow Regulator; June, 1926
ID: SIL7-17-01
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Vol. I, Fig. 159. Details of Top of Combustion Chamber
ID: SIL7-17-02
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Vol. I, Fig. 160. Details of Top of Combustion Chamber
ID: SIL7-17-03
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Vol. I, Fig. 161. Details of Top of Combusion Chamber
ID: SIL7-17-04
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Vol. I , Fig. 162. Entrance Pipes for Fuel
ID: SIL7-17-05
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Vol. I , Fig. 171. Top of Combustion Chamber, showing Oxygen Delivery Tubes
ID: SIL7-17-06
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Vol. I , Fig. 172. Top of Combustion Chamber
ID: SIL7-17-07
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Vol. I , Fig. 185. Assembling Rocket - Complete Piping System
ID: SIL7-17-08
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