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160 MM Solid Rocket Motor (EPDM/APCP)
The 160 MM Solid Rocket Motor is a tactical solid-propellant motor designed for rockets and missiles requiring high thrust and reliable performance. With a motor diameter of approximately 160 mm, this type of motor is commonly used in small-to-medium tactical applications where rapid acceleration and sustained flight are required.
Key Details:
Category: Solid Rocket / Tactical Missile Propulsion System
Motor Diameter:
160 mm Solid Rocket Motor: Designed for tactical rockets or
missiles that require high-thrust propulsion and durable performance.
Description:
Structure: The motor features a durable casing containing a
cast solid propellant grain, with internal insulation made of EPDM
(Ethylene Propylene Diene Monomer) rubber to manage combustion heat.
The propellant grain is designed for consistent burn characteristics
and reliable thrust output.
Propellant Composition: Typically based on Ammonium Perchlorate
Composite Propellant (APCP). Standard components include ammonium
perchlorate as the oxidizer, aluminum powder as fuel, and polymer
binders such as hydroxyl-terminated polybutadiene (HTPB) or
polybutadiene acrylonitrile (PBAN).
Operational Design: Provides a stable, high-thrust burn for
tactical applications, suitable for long-term storage and ready
deployment in defense systems.
Common Uses:
- Tactical Missile Propulsion: Serves as a primary propulsion unit for small-to-medium tactical rockets and missiles.
- Defense Applications: Designed for use in military defense systems requiring high reliability and rapid launch capabilities.
- Research and Testing: Can be used in experimental or controlled testing environments for solid rocket motors.
Operational Features:
Solid-propellant design with EPDM insulation, durable metal casing,
consistent thrust output, reliable ignition, and suitable for long-term
storage in tactical or defense applications.
Contact us at: info@sae-group.net