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本文提出了一种推力可调的固体火箭发动机的设想方案。它将通过采用负压力指数推进剂来实现。文中讨论了这一技术的可实行性和调节的特性。还指出了负压力指数推进剂的其它优点。
In this paper, a proposal of a thrust adjustable solid rocket motor is proposed. It will be achieved by using negative pressure index propellants. The article discusses the feasibility of this technology and regulatory features. Other advantages of negative pressure index propellants are also pointed out.