Integrated Rocket Ramjet

To design an integrated rocket ramjet. The emphasis on designing a unique nosecone to function dually as an inlet for the ramjet, as well as a removable diaphragm between the ramjet engine and the solid rocket propellant.

Deliverables
The deliverables for this project include; a detailed design for an adjustable nosecone and diaphragm that utilizes aerodynamics, a quarter cut out model showing the functionality of the integrated ramjet, and a working model of the rocket that can be used for future testing.

Document Archive
[[Media: IRR_(MMT)_10_21_15.docx|Meeting Minutes]]