ULTRA SMALL MATRIX JET ENGINE ON THE BASIS OF SILICON MEMS TECHNOLOGY
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ENGINE DESIGN
The engine consists of several units:
- nozzle block
- ignition module
- section of combustion chambers filled with fuel
TECHNICAL CHARACTERISTICS
Number of engines in the matrix, pieces | 25 |
Engine matrix mass, g, not more | 25 |
Pulse of a single engine, mn·s | 40 |
Basic structural material | silicon |
Fuel | glycidylazide polymer |
DEVELOPER
R&D Lab 4.8 «Applied plasmonics»
CONTACTS
6, P. Brovki str., 220013, Minsk, Republic of Belarus
☏ +375 17 293 88 43
🖷 +375 17 390 96 28
🖂 eugene.chubenko@bsuir.by
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