METHOD OF TESTING THE EFFICIENCY OF ESISTOJET THRUSTERS WITH REMODELED NOZZLE AND FLOW CHAMBER DESIGNS

Abstract

ABSTRACT A method (100) for testing the efficiency of ESISTOJET thrusters with remodeled nozzle and flow chamber designs comprising: integrating advanced diagnostic tools to monitor thruster performance; utilizing real-time data to adjust thruster parameters for optimal efficiency; implementing precise control mechanisms to enhance fuel consumption and thrust output; and verifying the optimized performance through systematic testing and validation.

Specification

Description:FIELD OF THE DISCLOSURE
[0001] This invention generally relates to a field of aerospace engineering, and in particular, to a method for testing an ESISTOJET thruster with a remodeled nozzle and flow chamber design. The invention aims to provide a novel and efficient testing method for these thrusters, which are known for their applications in propulsion systems and research in advanced thruster technology.
BACKGROUND

[0002] The subject matter discussed in the background section should not be assumed to be prior art merely as a result of its mention in the background section. Similarly, a problem mentioned in the background section or associated with the subject matter of the background section should not be assumed to have been previously recognized in the prior art. The subject matter in the background section merely represents different approaches, which in and of themselves may also correspond to implementations of the claimed technology.
[0003] ESISTOJET thrusters are renowned for their simplicity, ro , Claims:1. A method (100) for testing the efficiency of ESISTOJET thrusters with remodeled nozzle and flow chamber designs comprising:
integrating advanced diagnostic tools to monitor thruster performance;
utilizing real-time data to adjust thruster parameters for optimal efficiency;
implementing precise control mechanisms to enhance fuel consumption and thrust output; and
verifying the optimized performance through systematic testing and validation.

2. The method (100) as claimed in claim 1, wherein the advanced diagnostic tools include high-speed cameras and pressure sensors.

3. The method (100) as claimed in claim 1, wherein the thruster parameters adjusted include fuel injection rate, ignition timing, and exhaust nozzle configuration.

4. The method (100) as claimed in claim 1, wherein the systematic testing and validation include thrust measurements, fuel efficiency analysis, and thermal management assessments.

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