Experimental Study on Thrust Characteristics of Airspace Laser Propulsion Engine

Ageichik, A. A.; Egorov, M. S.; Rezunkov, Yu. A.; Safronov, A. L.; Stepanov, V. V.

doi:10.1063/1.1720985

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Cited by 14 publications

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“…Atmospheric parameters (atmospheric density, dynamic viscosity, specific heat capacity and thermal conductivity) are calculated using USSA76 atmospheric model [4] . 2 [10.0320.58…”

Section: Tdcvs ρ ==mentioning

confidence: 99%

Study on radiation power density effects on flight performance

Jin¹,

Hong²,

Wang³

2015

Proceedings of the 5th International Conference on Advanced Design and Manufacturing Engineering

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KEYWORD: Laser, UAV, Radiation, Power density, Maximum level flying speed ABSTRACT: Laser-motive UAV (unmanned aerial vehicles) is a new concept UAV. Based on analysis of conservation equation of photoelectric conversion irradiated by laser energy, UAV load's demand for power density and heat convection balance, a model is established to analyze the relationship between UAV maximum level flying speed, maximum wing loading and laser irradiation power density, propulsion system output power, photovoltaic cells operating temperature, and further a method is proposed to calculate and analyze UAV flying height, maximum level flying speed and maximum wing loading, etc. The calculation and analysis method proposed in this thesis provides basis for the design and analysis of Laser-motive UAV.

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“…Atmospheric parameters (atmospheric density, dynamic viscosity, specific heat capacity and thermal conductivity) are calculated using USSA76 atmospheric model [4] . 2 [10.0320.58…”

Section: Tdcvs ρ ==mentioning

confidence: 99%