Requirement	Description	Component	Compliance
3.1	Dual Deploy CONOPS	Architecture	Vehicle is Single-Separation Dual-Deploy
3.1.1	Apogee Event	Avionics	System can accurately detect Apogee
3.1.1	Drogue Descent Rate	DGB Parachute	Descent velocity is between 75-150 ft/s. Compliance is TBD
3.1.2	Main Event	Avionics	Event Shall be no higher than 1500 ft AGL. Exemption Obtained. 2,000 ft AGL acceptable for larger parachute
3.1.2	Main Descent Rate	Main Parachute	Landing velocity is less than 30 ft/s.
3.1.4	Torsion Relief	Swivels	Swivels are implemented to relieve recovery system to airframe torsion
3.1.5	Drogue Color	DGB Parachute	Drogue is orange and white
3.1.5	Main Color	Main Parachute	Main Is red and black.
3.5 (4.0)	Energetic Devices	Firebolt	TBD
3.5 (4.0)	Energetic Devices	Tender Descender	TBD
3.6	Testing Compliance	Procedures	EHS and MIT Facilities procedures followed during all testing
3.6.1	Successful Ground Test	Architecture	Flight components have a successful ground test prior to flight
3.6.2	Successful Flight Test	Architecture	Flight Test Indefinitely Postponed
4.2	SRAD Pressure Vessel	Piston	TBD
6.2.2	Recovery Attachment Points	U-Bolts	U-bolt made of steel other than stainless steel

The design considerations associated the Hermes recovery system are summarized in the following pages:

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