Sub-orbital rocket minimum viable product

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[ Payload - audio/video equipment]

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Technical description and specifications

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• Mass: up to 20kg (44 lb)

• Fuel mass: up to 45kg (99 lb)

• Full mass: up to 65kg (143 lb)

• Duration: 45 sec

• Approximate flight altitude: 12km (7.5 nm)

• Fuel: peroxide hydrogen 85% (or higher)

• The fuel supply system - pressure fed system.

• Guidance system – raspberry Pi 4 + grid fins.

• Rescue system - parachute

• Engine thrust - 100kgs (220 lbf)

• Specific impulse - 120 sec

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