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.

Background
Currently there are two options for a ramjet engine to function. ONE: Requires the use of a jet to obtain the proper speed and altitude to meet the design requirements for the ramjet to function. TWO: The ramjet is attached to a booster rocket, which will fall off once the design requirements are meet. We will be creating a third approach that will allow for ramjet flight.

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: Meeting_Minutes2.0.pdf|Meeting Minutes]]