Luminis
The first airframe designed around its payload rather than the other way round.
What it did.
Figures come from the onboard flight computer.
- Apogee
- Not publishedfeet above ground level
- Max velocity
- Not publishedat burnout
- Max acceleration
- Not publishedpeak, from flight data
- Length
- 2.8 m (110 in) overall, tip to tail
- Liftoff mass
- 16.8 kg dry / 22.6 kg wet fuelled, with payload
- Motor
- CTI 6800M3700-P designation and impulse class
- Recovery
- 2 ft drogue @ apogee · 12 ft main @ 1400 ft drogue and main configuration
- Result
- Not published
How it was made.
Luminis kept the 5 in fiberglass layout from Marauder II (Von Karman nose, three clipped-delta carbon fins) and added the team's first functional payload: an onboard camera for flight video. Dual-deploy recovery used a COTS EasyMini with Void Lake 4 as SRAD backup. It flew on a CTI 6800M3700-P (6,800 N·s).
At competition.




We hire first years.
We hire people who have never touched a rocket. Come ready to learn. We'll teach the rest.
Find us at Facultyfest on August 31, 12:30 to 17:00, or Clubsfest on September 14, 16:30 to 19:30 on the JHE field. Applications close September 18. You don't need to be an engineer: we need people on operations as much as on airframe.