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LRSAM / MRSAM / QRSAM Solid Propellant
The LRSAM, MRSAM, and QRSAM systems use high-energy, smokeless solid fuel propellants, typically Composite Modified Double Base (CMDB) or similar formulations, housed in a single-stage rocket motor. This propellant delivers intense, fast-burning thrust for high-acceleration supersonic flight and rapid interception of aerial threats.
Chemical Formula & Composition (General):
- Oxidizer: Ammonium Perchlorate (NH4ClO4).
- Fuel: Aluminum powder (Al) for high-energy combustion.
- Binder: HTPB (Hydroxyl-Terminated Polybutadiene) or polyurethane to provide structural integrity and controlled burn rate.
Description:
The propellant is a solid, molded, rubbery composite cast into the missile's rocket motor. It is engineered for high-energy density, rapid combustion, and minimal smoke to reduce infrared and visual signatures during flight.
Use:
- Propulsion for supersonic surface-to-air missiles (SAMs) like LRSAM, MRSAM, and QRSAM.
- Enables quick-reaction interception of aircraft, helicopters, and other missiles at various ranges.
- High-acceleration, low-signature thrust ensures reliable engagement in tactical air defense scenarios.
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