The invention discloses a cooling-to-energy
aerospace engine. An ignition or energy emission device is arranged in an energy chamber of the cooling-to-energy
aerospace engine; small holes are distributed in the inner wall of the energy chamber and communicate with a working medium compression
regulator and a working medium constant-temperature storage box through working medium guide pipes; the energy chamber is connected with an inner spray
pipe and is provided with an inner
nozzle; temperature detectors are arranged on the outer
layers of the energy chamber and the inner spray
pipe and communicate with a temperature controller through temperature
signal wires; the energy chamber and the inner spray
pipe are sleeved with a cooling cover; a cavity is formed between the energy chamber and the inner spray pipe to form a sleeve type outer spray pipe and an outer
nozzle; small-hole spray pipes are distributed on the inner wall of the cooling cover; and one end of each small-hole spray pipeis connected with a
water pressure regulator and a constant-temperature water tank through cooling water pipes. According to the engine, the cooling cover, the pipelines and other devices convert heat dissipation into propulsion energy, the temperature of the energy chamber and the temperature of the inner spray pipe are greatly increased, and the
specific impulse is increased; the structure andthe control difficulty are reduced, repeated use is achieved, the size and the weight are reduced, the manufacturing, maintaining and using costs are low, and the engine is applicable to various spacetasks.