固体火箭发动机平衡压力唯一性探讨

RESEARCH ON THE NON-UNIQUENESS OF EQUIVALENT PRESSURE IN A SOLID ROCKET MOTOR

提出了催化燃烧双基推进剂在固体火箭发动机中可能出现几个平衡压力的看法。实验证实了此观点的正确性,并讨论了产生非唯一平衡压力的内在条件及外在原因。

A new concept that there could be more than one equivalent pressures in a solid rocket motor using double-base propellant has been put forward. This hypothesis has been confirmed by a few experiments. The authors have also discussed the conditions of existence of non-unique equivalent pressures.