Engineering:MAX-1 (spacecraft)

From HandWiki
MAX-1
ManufacturerCopenhagen Suborbitals
Country of originDenmark
Specifications
Spacecraft typeCrewed suborbital launch and reentry
Launch mass350 kg (770 lb)
Volume~600,000 cm3 (37,000 in3)
Power12/24V DC
Dimensions
Length4 m (13 ft)
Diameter64 cm (25 in)
Production
StatusAbandoned

The MAX-1 is a crewed spacecraft designed by Copenhagen Suborbitals.[1] It is named after American rocket engineer Maxime Faget. The MAX-1 is designed to be similar to the Mercury spacecraft.

For descent it would have used a parachute which deploys from the top of the spacecraft. The ingress/egress hatch is placed above the head of the astronaut and can be opened and closed from both the inside and outside using 8 pneumatic cylinders. MAX-1 was produced out of aluminium.

Basic Data

  • Mass: 350 kg (including astronaut)
  • Length: approx. 4 meters
  • Diameter: 64 cm
  • Internal atmosphere: 1 bar, atmospheric gas
  • Pressurized volume: approx. 600 liters
  • Unpressurized volume: N/A
  • Parachutes: 3 (1 drogue + 1 pilot + 1 main)
  • Parachute data: cross type, 145 m2 total
  • Heat-shield: N/A
  • Communication: N/A
  • Tracking: N/A
  • Power profile: 12/24V DC
  • GNC profile: IMU system
  • Coding protocol: RS422
  • Additional info: Personal parachute for panic egress.

External links

References