Sprinter — high-speed airframe testbed.

Sprinter is the Track 2 hardware: a Gen-3 rocket-profile aero testbed—built, electronics integrated, finishing electrical configuration before manual propulsion and stability trials. Guidance work happens on Scythe. Parameters on this page are design targets—not qualified field specs. Sprinter is not flying autonomously.

Sprinter Gen-3 high-speed aerodynamic testbed — matte black rocket fuselage with swept motor nacelles

Sprinter · Gen-3 High-Speed Aerodynamic Testbed — Ithaca Flight Lab

Sprinter (Gen-3) high-speed aero testbed.

Purpose-built projectile-profile flight article: swept quad layout, modular nosecone bay, rigid composite construction. Electronics are integrated; once electrical configuration is complete it will validate low-drag aerodynamics, motor thermals, and high closure speeds under manual flight.

  • Status · Electronics integrated / pre-flight configuration
  • Control · Manual — autonomy payload later
  • Convergence · After tethered rates on Scythe

Autonomy stack (YOLO + IBVS on Pi 5) stays on Scythe until Sprinter envelope work is complete.

Interactive CAD · Gen-3 Drag left / right

Loading airframe model…

Sprinter Gen-3 CAD twin.

The same geometry as the built airframe above. Drag to rotate around the vertical axis.

Gen-1 → Gen-3 design lineage →
Gen-1 airframe FEA · sim only
Gen-1 interceptor concept — finite element stress / heat map from simulation
Stress visualization from structural simulation — not flight hardware

Gen-1 airframe FEA concept.

Earlier notional interceptor studied in simulation—stress and load paths for structural iteration. Informed later airframe geometry; not the flight article above.

FEA / concept render only.

Recorded intercept scenario.

PX4 / Gazebo software-in-the-loop run shown on a plan position indicator display. Simulation only.

> SITL SIMULATION // ASSET: IC-001 // STATUS: INTERCEPT SCENARIO COMPLETE

Gen-1 design targets.

Notional parameters for a high-agility airframe model used in closed-loop guidance simulation against maneuvering UAS and mobile ground-target trajectories—stated as design targets, not qualified or field specifications.

90mph

Notional speed (sim)

12km

Notional range (sim)

<90s

Time to acquisition (sim)

~30Hz

Control loop design target

Sprinter and Scythe milestones live on one development timeline.