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250 SMITHSONIAN ANNALS OF FLIGHT tl , i • / .'| .L--'"'A1S « I :: * reliability and safety of the power plant. The work on the rocket aircraft was carried on at the design office headed by V. F. Bolkhovitinov, where an experimental model of the BI-1 rocket fighter (Figure 4) was designed and manufactured. The fighter Was fitted with a powerful nitric acidkerosene engine with thrust of over 1000 kg. During the war, in 1942, the BI-1 fighter was flown by the pilot G. Ya. Bakhchivandzhi. 0 Pilotless Winged Rockets The 06/1—the first winged rocket—was a smaller geometrical model of the RP-7 rocket aicraft. It was FICURE 2.—Layout of RP-218. 4 1t- fitted with an 09 oxygen engine having a maximum thrust of approximately 50 kg. The rocket weighed 30 kg. Research on the 06/I-06/III was guided by Ye. S. Shchetinkov. The rocket takeoff was similar to that of an aircraft, i.e., it was performed from horizontal guide rails. The winged rocket was expected to climb along an inclined trajectory (at an angle of about 60° to FIGURE 3.—a, Layout and b, tail surfaces of RP-318; c, rocket engine for the 318; d, RP-318-1 in flight, 28 February 1940.
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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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138 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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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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300 SMITHSONIAN ANNALS OF FLIGHT -
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Abbot, Dr. Charles Greely, 57-59, 6
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NUMBER 10 305 Mengering, Franz, 226
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NUMBER 10 307 Scherchevsky, Alexand
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