Technical Description
This invention relates to a solid propellant-based afterburner integrated with a gas turbine engine for vehicle propulsion.
Problems Addressed
- Lacks Compactness
- Inefficient Thrust
- Heavy Engine
- Complex Injection
- Extra Weight
- Limited Efficiency
- Bulky Design
Tech Features
- Compact Efficient Design
- Lightweight Better System
- Enhanced Thrust Capability
- Efficient Propellant Use
- Better Integration
- Enhanced Performance
Target Audience
- Aviation & Aerospace Industry
- Defense & Military Aviation Sector
- Space Research & Propulsion Agencies
- Gas Turbine & Jet Engine Manufacturers
- Research & Development
Tech ID: P04-1589 TRL 5 Patent Status: Granted Available For Exclusive and Non-exclusive License
