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International Journal of Energetic Materials and Chemical Propulsion
ESCI SJR: 0.142 SNIP: 0.16 CiteScore™: 0.29

ISSN Print: 2150-766X
ISSN Online: 2150-7678

International Journal of Energetic Materials and Chemical Propulsion

DOI: 10.1615/IntJEnergeticMaterialsChemProp.2018024455
pages 115-123

IGNITION AND COMBUSTION CHARACTERISTICS OF A MICRO-ELECTROMECHANICAL SYSTEM (MEMS) PYROTECHNIC THRUSTER FOR MICRO PROPULSION APPLICATIONS

Harshit Shukla
Department of Space Engineering and Rocketry, Birla Institute of Technology, Mesra, Ranchi, 835215, India
Gusain Rajesh Singh Nandan
Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram, 695022, India
Priyanka Shukla
Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram, 695022, India
Vinod Kumar
Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram, 695022, India
Mohan Varma
Department of Space Engineering and Rocketry, Birla Institute of Technology, Mesra, Ranchi, 835215, India

ABSTRACT

A functional micro-electromechanical system (MEMS)-based micro-thruster using boron–potassium nitrate pyrotechnic composition with an electron beam deposited platinum heater has been characterized for reproducible ignition and sustained combustion. Configuration of the device, assembly process, and the energetic material were selected based on a detailed study involving a series of ignition tests. Successful ignition was achieved for the chosen configuration and the energetic material. The development demonstrated potential of such devices along with scalability for futuristic applications aimed toward downsizing of micro-spacecraft propulsion systems.


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