This web page presents the test report detailing the first static test (KDX-001) conducted on the Kappa-DX rocket motor, as well as post-test analysis.
这个网页介绍了测试报告，详细说明第一静力试验(kdx - 001)上进行了河童的dx火箭发动机，以及后的测试分析。
The pressure-time trace from the KDX-002 static test of the Kappa-DX rocket motor will be used to estimate the propellant burn rate, with the results compared to Strand Burner data .
压力-时间痕量从kdx - 002静力试验的河童的DX火箭发动机将被用来估计推进剂燃烧率，与结果相比， 钢绞线燃烧器的数据 。
Figure 8 shows a comparison of the two static test results for the Kappa-SB motor with KN-Sorbitol propellant.
图8显示的比较两个静态测试结果为Kappa值锑电机千牛-山梨醇推进剂。
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