CBCHASE BISSELL
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ROCKETRY / SUPERSONIC DESIGN

CALYPSO-1 · Mach 1 rocket

A collaborative student rocket project targeting supersonic flight, recorded flight data, and successful recovery.

ANSYS analysisCustom fabricationFlight instrumentation
TIMEFRAMEFall 2026 — Ongoing
MY INVOLVEMENTCo-design, modeling & fabrication

The project

CALYPSO-1 is a collaborative project to design, build, and recover a student-built rocket that exceeds Mach 1. The design emphasizes low cost, custom fabrication, and recorded flight data. Robert Werner and I share the design, modeling, and fabrication work, collaborating across the full project.

Shared engineering work

01

Mission & requirements

The project targets flight above Mach 1 while maintaining stability and structural integrity. Additional objectives include recording altitude and velocity, capturing onboard video, GPS tracking, and dual-deployment recovery.

02

Design tradeoffs

We jointly develop the design, models, and fabrication approach. Our preliminary component budget compares candidate materials, parts, mass, and cost. The design considers a fiberglass airframe, G10 fiberglass fins, and a custom polycarbonate nose cone alongside flight instrumentation and recovery hardware.

03

Analysis & verification plan

The project materials include ANSYS flow visualizations. The documented test plan calls for flight and recovery-drift simulations, aerodynamic-load and structural analysis, component tests, final mass and center-of-gravity measurements, and comparison of flight data with predictions.

ANALYSIS IN PROGRESS

Visualizing the flow field.

Project CFD visualization showing a Mach-number contour around the rocket geometry
Mach-number contour from the CALYPSO-1 project materials. Simulation visualization; not measured flight performance. Select the image to inspect it at full size.

The flow-field image provides a view of the current analysis work. Its color scale represents local simulated flow conditions, not the rocket’s achieved flight speed.

THERMAL ANALYSIS

Transient temperature simulations.

Thermal cross-section
Equalized thermal cross-section

STATUS & EVIDENCE

In development. Supersonic flight and successful recovery are project objectives. The current portfolio presents design documentation and simulation material, rather than a completed flight-test result.

KEEP EXPLORING

Thrust vector control

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