Emerging Trends in Instrumentation in Rocket Motor Testing
Abstract
Rocket motors are designed, developed, and evaluated for performance, and after repeated tests, are qualified for use in a spacecraft or missile system. Comprehensive instrumentation measurement plan is made to record physical parameters during evaluation and testing. In the last thirty years, a revolution has happened in the field of electronics that has benefited instrumentation in terms of accuracy, bandwidth, capacity, reliability and analysis. This paper describes the improvements in instrumentation that have happened in the field of rocket motor testing over a period of last three decades.
Defence Science Journal, Vol. 65, No. 1, January 2015, pp.63-69, DOI:http://dx.doi.org/10.14429/dsj.65.7949
- 3T, LP Rocket Engine ready for test
- 3T, LP Rocket Engine under test
- Data Acquisition Facility and Test Bed
- Component of Instrumentation system
- Types of flow meter
- Types of load cell
- Types of Pressure Transducer
- K-Type Thermocouple
- Schematic of Centralised Data Acquisition Facility installed in 1987
- Sample of UV record with chemical sprayed
- Thrust and Pressure profile of a Rocket
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