LIVE · 2026 INTERCOLLEGIATE ROCKET ENGINEERING COMPETITION
TEAM 02 · GRINNELL COLLEGE · 10K COTS SOLID CATEGORY
Grinnell College Logo

Flying Squirrel Rising.

A 10,000-foot class sounding rocket designed, built, and flown by undergraduates at Grinnell College. Fiberglass airframe, L-class solid motor, dual-deployment recovery, and a functional vibration-isolation payload — engineered from a small liberal-arts campus to the launch rail at IREC 2026.

Predicted Apogee
6,480 ft AGL
Max Velocity
232 m/s
Max Acceleration
12 g
Liftoff Weight
10.398 kg
Total Impulse
2,714 N·s
Rail Departure
30.7 m/s
01 // MISSION

A first-year team with a disciplined flight plan.

Grinnell is a small liberal-arts college without a dedicated aerospace program. Our team is physics majors, mathematicians and natural-science students who organized this project as a student-led initiative under faculty oversight. We chose a proven COTS airframe and motor so our limited build time is spent where it matters: quality assembly, thorough ground testing, and careful documentation.

Weekly Meetings
Saturdays · 2PM
Sundays · 6PM
Noyce Science Center · Room 0234
Faculty Supervisor
Prof. Shanshan Rodriguez
Department of Physics · Grinnell College
Team Mentor · Flyer of Record
Lanie Cross
Tripoli #5008 · Level 3 Certified
02 // VEHICLE

The Flying Squirrel — a conservative, well-understood machine.

Airframe & Structures

Built around the Dominator 4 COTS fiberglass kit — 4-inch filament-wound body tubes, a fiberglass nosecone with a metal tip, and a 54 mm motor mount. Three trapezoidal fiberglass fins bonded through the airframe with J-B Weld Steel Reinforced Epoxy. Fin flutter analysis gives an estimated flutter velocity of 516 m/s — a 122% safety margin over predicted max velocity.

Propulsion

A single AeroTech L1000W-14A single-use solid motor. 75 mm diameter, 2,714 N·s total impulse — well below the IREC 40,960 N·s cap. The L1000W reliably produces the 30.7 m/s rail-departure velocity required on the 5.18 m ESRA rail at our liftoff weight.

Recovery

Single-airframe dual-deployment. Drogue deploys at apogee; main at 500 ft AGL. Two redundant COTS altimeters — AltusMetrum TeleMega v3.0 primary and EasyMini v2.1 backup — command black-powder charges. Simulated touchdown velocity under main: 6.16 m/s.

Payload — Vibration Isolation Experiment

A 2.0 kg functional scientific payload measuring vibration-isolation performance of candidate packaging materials. Five three-axis accelerometer channels arranged radially, each surrounded by a different test material — vibration damping film, closed-cell packing foam, corrugated cardboard, and a bare control.

Avionics & Tracking

TeleMega built-in 70 cm GPS transmitter at 16 dBm. Ground station: AltusMetrum TeleBT receiver, laptop running AltOS, Arrow 3-element Yagi antenna.

Length
2.56 m
Diameter
102 mm
Fins
3 × fiberglass
Stability
3.1 cal
Motor
AeroTech L1000W
Airframe
Dominator 4
03 // CONOPS

Six phases from pad to touchdown.

Single-stage, single-motor, dual-deployment profile. Every transition is guarded by redundant altimeters.

01
Prelaunch
Assembly, continuity checks, charge installation away from the pad. Igniter installed at the rail under RSO supervision.
02
Ignition + Boost
L1000W fires. Rail departure at 30.7 m/s off the 5.18 m ESRA rail. 12 g peak acceleration during boost phase.
03
Coast
Unpowered coast to apogee. TeleMega and EasyMini independently detect apogee via barometric + accelerometer fusion.
04
Drogue
1.1 g primary charge fires at apogee. EasyMini backup at 1.5 g if needed. ~20 m/s drogue descent.
05
Main
At 500 ft AGL, 0.67 g primary main charge separates nosecone from payload bay. Descent to 6.16 m/s under main.
06
Recovery
Single tethered assembly touches down. Team locates via TeleMega GPS. Safing, inspection, and payload download on site.

Milestones

FALL 2025
Airframe assembly & epoxy cure
Complete
WINTER 2026
Avionics bench test — multiple simulated flight profiles
Complete
SPRING 2026
Recovery ground test — primary + backup ejection charges
In Progress
SPRING 2026
FCC amateur radio license issuance
In Progress
MAY 15, 2026
Technical Report submission to IREC
Upcoming
JUNE 2026
IREC launch window — Midland, TX
Upcoming
04 // TEAM

Seven students. One rocket.

Undergraduates from physics, mathematics and the natural sciences. No aerospace department – just hands-on engineering.

SR

Sophia Ramalli

Student Lead / President
Physics Major
SS

Shira Sheppard

Alt Student Lead / VP
General Science – Biology
HL

Hanson Liu

Treasurer
Physics Major
HE

Harrison Elliott

Payload Lead
Physics Major
EL

Eti-Abasi Laurel

Avionics Lead
Math & Physics
CD

Carmela Davidson

Recovery Lead
Physics Major
SR

Stephany Ronquillo

Recovery Lead
Physics Major
05 // JOIN

Want to build rockets?

You don’t need to be a physics major. You don’t need prior experience. You need to show up, learn a solder iron, and be excited about things that go fast. Right now we’re working on the biggest thing we’ve ever done: IREC 2026.

Email the Rocket Team→ @grinnellrocket

Grinnell College · Grinnell, Iowa · United States. A student-led rocketry group competing in the 2026 Intercollegiate Rocket Engineering Competition.
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© 2026 GRINNELL ROCKET TEAM · TEAM 02 · IREC 2026 · AD ASTRA