| 摘要 |
<p>An enhanced combustion rocket engine system (100), involving at least one primary propellant tank (110) adapted to accommodate a primary propellant (111) in at least one of a solid state, a transition melting state, and a molten state and to deliver the primary propellant (111) in the molten state, at least one secondary propellant tank adapted to accommodate a secondary propellant in a liquid state; and at least one rocket engine (140), the at least one rocket engine (140) adapted to receive the primary propellant (111) from the at least one primary propellant tank (110) in a temperature range of at least approximately above an ambient temperature, to receive the secondary propellant (121) from the at least one secondary propellant tank (120) in a temperature range of at least approximately below an ambient temperature; and exothermically react the primary and secondary propellants (111, 121) for effecting combustion to provide thrust.</p> |
