| 摘要 |
The flying body includes a body ( 100 a), a lift engine ( 102 a 1 ), and reaction control engines. The lift engine includes, a gas generator ( 200 a 1 ) for generating a turbine driving gas, a first thrust device ( 204 a 1, 208 a 1, 210 a 1 ) for providing a power by the turbine driving gas and exhausting a gas ( 20 a 1 ) in a predetermined direction to generate a first thrust force, a second thrust device ( 214 a 1, 218 a 1, 220 a 1 ) driven by the power to suck and compress a surrounding gas ( 21 a 1 ) and to accelerate and exhaust the surrounding gas substantially in a direction of a flow of the gas exhausted by the first thrust device to generate a second thrust force to be added to the first thrust force. The gas generator generates a gas by using a raw material ( 10, 11 a) for gas generation carried by the flying body. The first thrust device has a turbine ( 204 a 1, 208 a 1 ) for obtaining a rotational force, and the second thrust device has a fan ( 214 a 1, 218 a 1 ) driven by the rotational force obtained by the turbine, and a nozzle ( 222 a 1 ) in a downstream of the fan.
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