Self-Propelled Projectiles TRIZ Cases
- Integrated Actuation System for Missile Thrust Vector Control
An integrated actuation system directs propellant through internal and external outlets to control missile thrust vector and attitude.
- Silicone Rubber Charge Holder with Metal Wire Reinforcement
Embedding metal wires in silicone rubber charge holders matches thermal expansion coefficients to confinement tubes, resolving contraction issues.
- Compression Spring Cam Wing Deploy Initiator
A compression spring drives a cam to force guidance wings outward through fuselage slots.
- Folding Articulating Wing Locking Mechanism
Tapered locking plunger secured by a coiled compression spring engages a mating surface on the wing assembly.
- Ejectable Aft Fin Housing for Projectile Stabilization
An ejectable aft fin housing assembly alters the center of pressure to stabilize small form factor aero-bodies at high angles of attack before ejection.
- Rotational Lock Mechanism for Control Surfaces
Integrated locking members on the output gear couple with a lock plate to prevent control surface movement under high aerodynamic loading.
- Separable Missile Fairing for Terminal Agility
Segmented fairing shells jettison sequentially to eliminate residual mass, restoring terminal vehicle agility while maintaining ascent protection.
- Nose Cone Divert Control System for Rocket Propulsion
A nose cone divert control system relocates attitude management hardware into the forward section to optimize nozzle slew angles.
- Projectile Flare Assembly with Dynamic Petal Actuation
A flare assembly uses an actuating mechanism to deploy petals for aerodynamic control.