科技报告详细信息
| Key Performance Parameters for Future NATO Hybrid/Electric Military Air Vehicles | |
| Dyson, Rodger | |
| 关键词: FLY BY WIRE CONTROL; TURBOGENERATORS; HYBRID PROPULSION; ENGINE AIRFRAME INTEGRATION; PROPULSIVE EFFICIENCY; HEAT ENGINES; STIRLING ENGINES; COMBUSTION STABILITY; NORTH ATLANTIC TREATY ORGANIZATION (NATO); | |
| RP-ID : GRC-E-DAA-TN60655 | |
| 学科分类：航空航天科学 | |
| 美国|英语 | |
| 来源: NASA Technical Reports Server | |
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【 摘 要 】
Presentation on power, propulsion, thermal, airframe integration, basic technology performance requirements, power options, efficiencies and limits.
【 预 览 】
| Files | Size | Format | View |
|---|---|---|---|
| 20180006764.pdf | 2675KB |  download |
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