Launch Systems TRIZ Cases
- Auxiliary Payload Support Unit for Launch Vehicle
A modular auxiliary payload support unit coordinates secondary spacecraft release via a single cable interface.
- First Stage Booster Recovery via Aerodynamic Turn and Reignition
A first stage booster uses aerodynamic flight controls to turn back toward the launch site before reigniting its rocket engine for a powered descent.
- Exoskeletal Launch Support Structure for Spacecraft
An exoskeletal launch support structure carries primary loads during ascent.
- Space Debris Interception Vehicle Elliptical Orbit Capture
A dedicated interception vehicle engages space debris using mechanical capture means to transition into a lower elliptical orbit.
- Satellite Release Safety Subsystem for Orbital Transport
Safety subsystem activates actuator members to open release doors and exert separation thrust on satellites during orbital deployment.
- Satellite Deployment Base with Synchronized Release Mechanisms
A movable base structure secures a space structure using synchronized release mechanisms that engage features during deployment.
- Kinetic Energy Storage Tether for Orbital Momentum Transfer
A kinetic energy storage vehicle uses a tether to transfer linear momentum to a target space vehicle.
- Reusable Launch Vehicle Stage with Perpendicular Fans
A reusable launch vehicle stage uses fans with rotational axes perpendicular to the central longitudinal axis to generate lift during landing.