OHKLA Design Task Tree
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(Redirected from OHKLA Design Tasks)
This page is part of an implementation of the CSTART Engineering Process. Anyone can edit it, but it should only be modified in accordance with the procedures and guidelines of the Process. Please check before editing if you are in doubt.
- Propulsion
- Hybrid rocket engine development
- Propellant choice
- Fuel grain geometry
- Oxidiser tank design
- Combustion chamber design
- Chamber material
- Injector manifold design
- Chamber material
- Ignition system design
- Exhaust nozzle design
- Nozzle cooling mechanism
- Nozzle material
- Nozzle shape
- Propellant choice
- Static Testing
- Static testing rig
- Sensors and supporting network
- Hybrid rocket engine development
- Structure
- Nose cone design
- Stabiliser fins design
- Fin material
- Fin shape
- Number of fins
- Fin cant angle
- Avionics
- Controller
- Data sensors
- Data storage
- Communications
- Cameras?
- Recovery
- Parachute choice/design
- Parachute release mechanism design
- Launch support hardware
- Launch pad design
- Launch tower design
- Operational
- Launch site
- Legal
- Launch license/permit requirements
- Safety
