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/ Technical DivisionDRACO Division

Airbrakes & Apogee Control

Active Drag ControlServo ActuationOnboard Control LogicBench & Flight Testing
/ OverviewThe Apogee Problem

A rocket cannot be told to stop climbing

Once the motor burns out, the vehicle coasts. Everything that decides how high it ends up — motor performance, mass, wind, air density — was fixed before it left the rail. Unless something can add drag on the way up.

That is what this division builds: a set of flaps that open into the airflow during coast, under onboard control, to trade excess energy for accuracy. It gives the vehicle a way to correct toward its target apogee instead of simply arriving wherever physics leaves it.

First integrated on Koeia, the 2026 vehicle

/ 01Integration

Where the system lives

Airbrakes is not a bolt-on. The mechanism occupies a section of the airframe between the motor and the recovery bay, and every millimetre of that volume is shared with other divisions.

Fig. AAft airframe assembly
CAD section view of the aft airframe assembly, with the deployed airbrake flaps visible mid-body ahead of the fin can
Section view of the aft airframe. The flaps sit mid-body, forward of the fin can — deployed here for clarity.
Fig. BMechanism assembly
CAD render of the airbrakes module with its flaps deployed, a controller board mounted on the upper deck, and the drive screw visible inside the housing

One actuator, symmetric deployment

The flaps are linked so a single drive extends all of them together. That symmetry is not a convenience — asymmetric drag would push the vehicle off its heading, so the mechanism is designed to make uneven deployment mechanically difficult rather than merely unlikely.

The controller mounts directly to the module, so the sensing, the decision, and the hardware being commanded all travel as one assembly.

/ 02The Control Loop

Sense → decide → actuate, onboard

During coast the system runs a closed loop with no human in it. Each stage below is a real part of the vehicle, not a diagram.

SensePCB layout
Circuit board layout for the ACS PCB 2026 v1, showing footprints for a BMP390 barometric sensor, an ICM-20948 IMU, and a servo-driver header
ACS PCB, 2026 revision 1 — barometer, IMU, and servo-driver headers on a single board.
01Sense

Know where you are, and how fast

The onboard board carries a barometric pressure sensor and an inertial measurement unit, so the system can estimate altitude and motion continuously through the burn and coast phases.

A DRACO member writing the airbrakes control software on a laptop
Control software development — the decision layer between the sensors and the servo.
02Decide

Compare to the target, every cycle

Onboard logic takes that state estimate, projects where the vehicle would coast to if it did nothing, and decides how far the flaps should be open right now. It runs unattended — there is no link to the ground during the seconds that matter.

Bench test setup with the airbrakes mechanism wired to a single-board computer, breadboard, and battery on a workbench
Bench rig — mechanism, controller, and power wired together before anything flies.
03Actuate

Move the flaps, add the drag

A servo drives the linkage that pushes the flaps out into the airflow. More surface means more drag, which means less remaining altitude — the only control authority the vehicle has after the motor burns out.

/ 03How The Work Divides

Built here, validated together

Apogee control sits on the boundary between mechanism and aerodynamics, so the division's scope is drawn deliberately.

Airbrakes & Apogee Control owns

  • The drag control mechanism and its structure
  • Actuation and servo control
  • Onboard control hardware and logic
  • Sensors and software/hardware integration
  • Bench and ground testing of the system

Flight Performance provides

  • Computational fluid dynamics (CFD)
  • RocketPy and Monte Carlo analysis
  • Trajectory and apogee prediction
  • Aerodynamic validation of the drag model

The two divisions work the same problem from opposite ends: one builds the thing that changes the drag, the other predicts what changing it will do.

/ ScopeCore Responsibilities

What this division owns

01

Active drag control system & airbrake mechanism

The deployable surfaces themselves, and the linkage that drives them from a single actuator.

02

Actuation system & servo control

Sizing and commanding the actuator that has to move under aerodynamic load, repeatably.

03

Onboard control logic & hardware

The board, the firmware, and the decision loop that runs with no one watching.

04

Sensors & software/hardware integration

Making the electrical and mechanical halves behave as one system inside a body tube.

05

Testing, with Flight Performance for aerodynamic validation

Bench and ground testing here; simulation and aerodynamic validation in partnership with Flight Performance.

/ StackTools & Skills

What members work with

  • Control systems
  • Servo actuation
  • Embedded electronics & sensors
  • Mechanical design
  • Software/hardware integration
/ Why It MattersImpact on DRACO

The bottom line

Airbrakes lets DRACO actively control its flight, closing the gap between predicted and achieved apogee — a defining capability for competitive performance, first integrated on the 2026 vehicle, Koeia.

An astronaut performing a spacewalk above Earth

/ Join Airbrakes

Control Is Something You Build

Mechanism design, embedded electronics, and control software in one division — with hardware that has to make its own decisions in flight, with no one able to intervene.