《AIAA-81-1371 COMPARISONS OF ADVANCED HYDROCARBON ROCKET ENGINES FOR EARTH-TO-ORBIT VEHICLES》求取 ⇩

作者	编者
出版	12
参考页数	✅ 真实服务非骗流量 ❤️
出版时间	没有确切时间的资料
ISBN号	无 — 违规投诉 / 求助条款
PDF编号	817775138（学习资料勿作它用）
求助格式	扫描PDF（若分多册发行，每次仅能受理1册）

AIAA-81-1371 COMPARISONS OF ADVANCED HYDROCARBON ROCKET ENGINES FOR EARTH-TO-ORBIT VEHICLES PDF电子版封面

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高度相关资料

: AIAA-81-1363 MULTI-MISSION V/STOL WITH VECTORED THRUST ENGINES; 7

: AIAA-81-1610 THRUST IMBALANCE OF THE SPACE SHUTTLE SOLID ROCKET MOTORS; 6

: AIAA-81-1592 A COMPACT INSTALLATION FOR TESTING VECTORED-THRUST ENGINES; 9

: AIAA-81-1550 ASSESSMENT OF FUTURE SOLID ROCKET MOTOR FLIGHT INSTRUMENTATION/DATA NEEDS; 9

: AIAA-81-1549 ADVANCED SOLID PROPELLANT ROCKET MOTOR FLIGHT INSTRUMENTATION; 11

: AIAA-81-1546 SERVICE LIFE ANALYSIS OF ROCKET MOTORS WITH INTERNAL GAS GENERATION; 3

: AIAA-81-1408 QUALIFICATION TEST RESULTS，5LBF（22 NEWTON）EARTH STORABLE BIPROPELLANT THRUSTER ROCKET E; 6

: AIAA-81-1402 DESIGN CONSIDERATIONS FOR DUTY CYCLE LIFE RELIABILITY OF SMALL LIMITED LIFE ENGINES; 3

: AIAA-81-1386 COMPUTATIONAL ANALYSIS OF COMBUSTION IN RECIRCULATING FLOW FOR ROCKET EXHAUSTS IN SUPER; 9

: AIAA-81-1385 SPACECRAFT CONTAMINATION FROM ROCKET EXHAUSTS; 9

: AIAA-81-1384 THE FLOW OF VERY SMALL ALUMINA PARTICLES IN A SOLID ROCKET PLUME; 5

: AIAA-81-1382 GENERALIZED FLOWFIELDS FOR APPROXIMATION OF ROCKET EXHAUST PLUME EFFECTS; 5

: AIAA-81-1377 STATUS REVIEW OF SOLID PROPELLANT ROCKET MOTOR PERFORMANCE PREDICTION; 10

: AIAA-81-1372 COMPONENT DESIGN AND PERFORMANCE EVALUATION OF A LIQUID PROPELLANT ROCKET ENGINE FOR EA; 8

: AIAA-81-1367 ENGINE USAGE PREDICTION FOR ADVANCED FIGHTER AIRCRAFT; 10

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