Valkyrie was CRT’s second student research and developed (SRAD) hybrid rocket and our competition rocket for the 2026 IREC. On the launch vehicle, we flew our SRAD parachute guidance system, BLiMS, for the second time successfully as well as SRAD airbrakes for the first time. The payload was a deployable 360º camera on an arm to take a video of Valkyrie's apogee and descent. At competition, Valkyrie placed third in the 10,000ft SRAD hybrid category.

3rd place 10k SRAD Hybrid

BliMS (Brake Line Manupulation System) is used to control the descent of the rocket by manipulating the brake lines of the ram air parafoil parachute, similar to how a skydiver controls their descent. BliMS is fully autonomous, using a PID controller to guide the rocket on a certain heading or to a GPS coordinate. This is the team's second time flying BliMS on a competition rocket, after flying it on Andromeda in 2025, several flights on a L3 test bed, and dropping it out of a plane.

Valkyrie's payload was a deployable 360º camera. It used an insta360 camera on a sero-actuated arm which deployed the camera at apogee through a slot in the airframe, acting as a selfie stick for the rocket. The camera was also positioned slightly outside of the rocket for flight to capture ascent before deployment.

The AV bay holds all the electronics to control the rocket, including the central fight computer, senseboard, and backplane. It commands the launch sequence of the motor, deployment of the chute, activation of other systems as well as logging flight data. All of the PCBs in the AV bay are SRAD, with a 3d printed board housing and machined bulkheads which interface with the wiring harness.

Airbrakes is a new system on Valkyrie. It consists of four metal plates that extend out of slots in the airframe to increase drag and lower the apogee of the rockt. The airbrakes deploy symmetrically, controlled by a single servo to ensure stability of the rocket. The airbrakes use live state estimation from flight data to determine when to deploy.

Valkyrie flew on a SRAD hybrid motor, delivering 1,385lbf of thrust and 20,000 Ns of impulse. It burns a mixture of liquid nitrous oxide and solid HTPB (hydroxyl-terminated polybutadiene) fuel. The motor was designed and built in-house by Cornell Rocketry, and is the second hybrid motor to be flown by the team.








Constructing a rocket sufficiently durable so that it may be launched, recovered, and re-launched repeatedly
Creating a communications system that will track the rocket and relay its flight information and location coordinates
Launching to precisely 10,000 feet above ground level
Reaching the required height with a one engine stage
Deploying a guided parafoil which ejects from the forward section during descent
