0.0 Rocket Requirements and Specification

 

Stakeholder Requirements Statements

1.0. Vehicle should fly to an altitude of 30 000 ft.

2.0. Vehicle should stay in constant communication [of telemetry] w/ ground through ConOPS stages 2-10.

3.0 Stable throughout flight

3.1 >100 ft/s Off the rail velocity

3.2 1.5 to 6 caliber - depends on wind condition constraint - value Should be double checked

4.0 Vehicle should be structurally sound throughout the flight

4.1

4.2 [Specific Load conditions]

5.0 Servicability throughout various stages

6.0 Vehicle should be recovered - With constraints from comp rules

7.0 Desert environmental requirements & robustness

8.0 Assembly process?

9.0 Safe states

10.0

 

  1.  

 

Parameters:

Design Spec: