Indian Space Research Organisation has successfully completed the test-firing of the Low Altitude Escape Motor (LEM) of Crew Escape System from Sriharikota, Andhra Pradesh.
Objective: Evaluation of motor ballistic parameters; Validation of motor subsystem performance.
LEM:
- It is a distinctive special purpose solid rocket motor.
- It has four reverse flow nozzles.
- It generates a maximum sea level thrust of 842 kN (nominal) with a burn time of 5.98 seconds (nominal).
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