Structural Hardware:
Nosetip
About the Component:
The nosetip is the foremost section of the rocket, designed to minimize aerodynamic drag and withstand aerodynamic heating, protecting internal payload during ascent.
Description:
- Material: Aluminum, Steel
- Dimensions: As per requirements
Nosecone
About the Component:
The nosecone provides the rocket’s aerodynamic profile, housing sensitive payloads while reducing drag.
Description:
- Material: Composite
- Geometry: Conical, Ellipsoidal, Ogive, Haack-Series, Power-Series
- Dimensions: As per requirements
- Shoulder: As per requirements
Airframe
About the Component:
The airframe is primary structural tube of rocket.
Description:
- Material: Composite, Aluminum
- Max Length: 4m (13.12 ft)
- Max Diameter: 0.5m (1.64 ft)
Body Coupler
About the Component:
The coupler serves as the connecting interface between rocket sections, ensuring secure alignment and load transfer across structural joints.
Description:
- Material: Composite, Metallic
- Dimensions: As per requirements
Fins and fixtures
About the Component:
Fins provide aerodynamic stability and guidance, ensuring the rocket maintains a straight flight path under varying atmospheric conditions.
Description:
- Material: Composite, Aluminum
- Dimensions: As per requirements
- Fin attachment: Fincan-bracket: fastened, welded; Composite fillet layup
Aft Coupler
About the Component:
The boat tail reduces base drag by smoothly transitioning rocket body diameter to the nozzle, improving aerodynamic efficiency and overall performance.
Description:
- Material: Composite, Reinforced plastics
- Dimensions: As per requirements