EXOROCKT Design Software by Aitken Werks

Choose your fuel, oxidizer, payload, and target apogee. EXOROCKET calculates the optimal rocket configuration and returns a CAD-ready design.

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EXOROCKET iterates through hundreds of rocket design configurations to find the mathematically optimal vehicle for your target apogee, payload, propellant choice, and mission requirements.

The result is a launch vehicle designed for maximum efficiency from the start, reducing the need for constant redesign and resizing throughout development. This saves R&D time and helps produce a rocket that is smaller, easier to build, easier to transport, and more cost-effective.

EXOROCKET optimizes:

  • Engine design
  • Thrust level
  • Fuel, oxidizer, and pressurant quantities
  • Tank sizing
  • Fin sizing
  • Overall vehicle geometry

The Software at a Glance

Plans

Single Simulation

Single Simulation

Student

Student

Enterprise

Enterprise

Outputs Generated from Exorocket Software

45, 000 Foot Collegiate Rocket

Inputs:

Thrust: 1875 N

Apogee: 13716 m (45,000 feet)

Best apogee AGL: 13712.417 m

RP-1 fuel used: 4.84 kg

Liquid Oxygen used: 12.58 kg

Karman Line Hydrogen Rocket

Thrust: 19000 N

Apogee: 100000 m

Liquid Hydrogen Fuel used: 76.89 kg

Liquid Oxygen Oxidizer used: 307.57 kg

Ultra Wide Alternative Rocket

Thrust 1500 N

Apogee: 10000 m

Ethanol Fuel used: 4.59 kg

Liquid Nitrous Oxide Oxidizer used: 24.82 kg