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Akronauts Rocket Design Team

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      • The Emergence Series
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Liquid Propulsion

VENM

Specifications:
  • Thrust: 400 lbf
  • Cooling: Ablative
  • Fuel: Ethanol
  • Oxidizer: Nitrous Oxide
See The Launch

HORNET

Specifications:
  • Thrust: 650 lbf
  • Cooling: Additive Regen
  • Fuel: Ethanol
  • Oxidizer: Nitrous Oxide
See The Hotfire

STINGER

Specifications:
  • Thrust: 2000 lbf
  • Cooling: Traditional Regen
  • Fuel: Ethanol
  • Oxidizer: Liquid Oxygen
See The Hotfire

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Want to help us reach our goals? Any contribution will help our team to continue innovating! Crazy about rocketry? We're always looking for more UA students to grow our team. All majors welcome and no experience necessary! Looking for updates? Check out our social medias to stay in touch and see what we're up to!
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