Split type omnibearing take-over laser booster
An all-round and separate technology, which is applied in the direction of combustion method, aerospace vehicle propulsion system device, combustion ignition, etc., can solve the problems of energy loss, limited adjustment range, and failure of optical mirror, so as to achieve small light loss and reduce development The effect of cost and simple structure
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[0027] The present invention has three structural forms, the structure adopting the single beam engine, the structure adopting the double beam single engine and the structure adopting the double beam double engine, which will be described in detail below.
[0028] As shown in Figure 3, the thruster of the present invention adopts a single-beam engine structure. It is composed of an optical system 1, a propellant tank 2, a combustion chamber 3 and a nozzle 4. The optical system 1 is located on the outer side of the combustion chamber 3. , And is connected to the solid body of the arrow body. A transparent circular laser incident window 5 is opened on the combustion chamber 3. The optical system 1 rotates around the laser incident window to realize receiving all the laser beams in the xz plane. When the laser beam passes vertically When the laser incident window 5 is concentrated and incident on the central position 6 of the combustion chamber 3, it ignites the propellant in the com...
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