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研究认为，较适宜的低压下贫氧推进剂燃速测试方法有靶线法、热电偶法、超声波法、发动机法和高速摄影法等。在低压贫氧推进剂燃速及燃速压强指数的数据处理过程中，应注意表压和绝对压强之间的差异，同时要注意选用合适的燃速规律。
The research suggests that the more suitable low oxygen propellant burning rate test methods are target line method, thermocouple method, ultrasonic method, engine method and high-speed photography method. In the process of data processing of low-pressure oxygen-poor propellant burning rate and burning rate pressure index, pay attention to the difference between gauge pressure and absolute pressure, meanwhile pay attention to choose proper burning rate law.