发明名称 |
SOLID-FUEL ROCKET ENGINE CHARGE |
摘要 |
FIELD: solid-fuel rocket engines and their charge. SUBSTANCE: rocket engine charge tightly fixed with casing and integral bottom is of cylindrical structure with central duct. It has tore front bottom. Annular projection is made on charge duct at front tore bottom end, its buttend surface being formed by two joined surfaces with curvature radii making up (0.02-0.05) and (005-0.01) of charge length. EFFECT: improved choice of horizontal-to-vertical ratio of fuel mass feed rate components to ensure its uniform flow over blind bottom surface on fuel mass feed end. 1 cl, 1 dwg
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申请公布号 |
RU2206778(C1) |
申请公布日期 |
2003.06.20 |
申请号 |
RU20010128237 |
申请日期 |
2001.10.18 |
申请人 |
"NAUCHNO-ISSLEDOVATEL'SKIJ INSTITUT POLIMERNYKH MATERIALOV";FEDERALNOE GUP |
发明人 |
AMARANTOV G.N.;BARANOV G.N.;SHAMRAEV V.JA.;TALALAEV A.P.;KOLESNIKOV V.I.;KHRENOV V.S.;KUZ'MITSKIJ G.EH.;FEDCHENKO N.N.;VRONSKIJ N.M.;GRINBERG S.I.;LISOVSKIJ V.M. |
分类号 |
F02K9/22;(IPC1-7):F02K9/22 |
主分类号 |
F02K9/22 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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