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 [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
Parameters:
Altitude
Dry mass
Propellant mass
Off-the-rail velocity
Descent Speed
Landing Speed
Design Spec: