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OMEN

What is OMEN?

OMEN was the 2023-2024 IREC rocket (intercollegiate rocket engineering competition) that competed in the international competition hosted in Spaceport America, New Mexico. OMEN was entered into the 10K COTS category.

Structures

  • The nose cone, body tubes, fins, boat tail, and all internal
    machined components being designed and manufactured by the team
  • Body tubes:
    • OMEN’s airframe consists of three SRAD body tubes
    • An outer diameter of 6.20 inches and an
      inner diameter of 6.00 inches
    • The team chose to utilize an X-winder
      filament winding machine to produce all three body tubes
  • Nose cone:
    • 3.5:1 tangent ogive nose cone due to its good performance in the subsonic and transonic
      regimes
  • Fins:
    • four fin configuration was chosen as it is easier to construct due to mirror symmetry across two
      perpendicular planes
    • Cut from 3/16 inch compressed carbon fiber sheets using an OMAX 5-axis waterjet cutter, and have a root chord of 12 inches and span 5.9 inches
    • Calculated the not-to-exceed fin flutter velocity to be 1456 ft/s 
  • Bulkheads:
    • Nose cone bulkhead
      • Designed to be weight-reduced from 1.908 oz to 1.25 oz
      • Tapered to fit the internal nose cone geometry
      • Purpose of holding the nose cone tip in place
    • Aft bulkhead
      • Weight-reduced design that reduces the weight from 11.8 oz to 6.23 oz
      • Includes a filleted circumference
    • Forward bulkhead
      • Differs with the interest of maximizing strain
      • Maintains an appropriate safety factor
      • Weightreduced from 12.5 oz to 5.51 oz

Payload

  • Payload name is Richie
  • CubeSat deployed at apogee
  • Objectives:
    • Testing an SRAD
      reefed parachute system
    • Measure the shock force of the deployment 
    • Disreef events using a load cell.

Avionics

  • Fully SRAD, modular and ethernet enabled flight computer
  • Flight computer will collect telemetry and sensor data
  • all-Derin avionics bay eases integration and increases durability
  • Avionics bay transmits GPS location from a Big Red Bee Beeline ona 70 cm APRS transmitter
  • Two RRC3 altimeters redundantly triggers the recovery system
Picture
Picture

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Contact

[email protected]
RIT Launch Initiative
73 Lomb Memorial Drive
Rochester, NY 14623

Meetings

Events Calendar

All Team Meeting:
Saturday - 11 a.m.
Institute Hall 1180

 
  • Home
  • About
    • Meetings
    • Meet the Team
  • Teams
    • IREC
    • Avionics
    • Liquid Propulsion
    • Solid Propulsion
    • Space Race
    • L1 Program
  • Projects
    • OTIS
    • Manhattan Project
    • Ad Astra
    • OMEN
    • The Backplane
    • Test Stand
    • Lukewarm Phoenix
    • Project Archive
  • References
    • Wiki
    • Publications
    • Trainings
  • Sponsors
  • Support Us