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火箭推进剂的实验室规模慢煮测试:缓慢加热推进剂(CRASH-P)测试的燃烧速率分析
JoVE Journal
Engineering
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JoVE Journal
Engineering
Laboratory Scale Slow Cook-Off Testing of Rocket Propellants: The Combustion Rate Analysis of a Slowly Heated Propellant (CRASH-P) Test
Please note that all translations are automatically generated.
Click here for the English version.
火箭推进剂的实验室规模慢煮测试:缓慢加热推进剂(CRASH-P)测试的燃烧速率分析
DOI:
10.3791/62216-v
•
06:52 min
•
February 06, 2021
•
Jonathan Essel
,
Andrew Nelson
,
Christopher Gray
,
Scott Sumner
,
Nathan Holl
1
Naval Air Warfare Center Weapons Division
Chapters
00:04
Introduction
01:14
Propellant Sample Installation
02:48
Test Instrumentation Setup
03:52
Data Acquisition and Test Cleanup
05:05
Results: Representative Combustion Rate Analysis of a Slowly Heated Propellant Test
06:03
Conclusion
Summary
Automatic Translation
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Automatic Translation
我们提出了一个实验室规模的固体火箭推进剂慢煮试验的协议,称为缓慢加热推进剂(CRASH-P)测试的燃烧速率分析。封闭式火箭推进剂在自动加热之前会缓慢加热,使用动态压力传感器测量烹饪温度和反应力。
Tags
Laboratory
Slow Cook-off
Rocket Propellants
CRASH-P Test
Combustion Rate Analysis
Slow Cook-off Reaction Violence
Rocket Propellant Development
Chemical Kinetics
Thermal Fluid Instrumentation
High Speed Data Acquisition
Temperature And Pressure Measurements
Propellant Sample Holder
Exothermic Reactions
Air Temperature
RTV
Chamber Cap
Retaining Head
Chamber Head
Chamber Retainer Clamps
Chamber End Plate
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