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Z. Zhang

Tier F Rocket

Carry an egg to 3,000 ft and bring it back

EXP-06
Org
UCLA ENGR 1 · Rocket Design
Role
Team lead · CAD & printing
Period
Fall 2025
2,916 ftapogee against a 3,000 ft target
~500 ft/s²peak acceleration
Intactegg recovered
1.0

Objective

I led a four-person team (named “Team Team”) from a Tier D trainer to a Tier F rocket on a G80T-13 motor. We laid up our own fiberglass airframe, redesigned the fins for drag, and built a nose-cone cushion that brought the egg back intact.

2.0

Work performed

  1. 2.1Modeled the rocket in SolidWorks and simulated flights in OpenRocket, first for the Tier D trainer, then for Tier F.
  2. 2.2Replaced the elliptical fins with swept, curved fins to cut drag at ~500 ft/s².
  3. 2.3Estimated the parachute deployment shock from nose-cone mass and shock-cord stiffness, then designed a two-density foam cushion in the nose cone, away from motor heat.
3.0

Specification

MotorG80T-13
AirframeTwo-layer fiberglass hand layup on a steel-pipe mandrel
Nose cone3D printed, minimum infill
AvionicsBMP388 altitude sensor with telemetry
ToolsSolidWorks · OpenRocket
4.0

Plates

Pl. 1Tier F recovery deploying: the red parachute streams out as the nose section separates on its shock cord, above the exhaust trail.
Pl. 2OpenRocket side profile on a G80T-13: 44 cm long, 6.3 cm diameter, 581 g with motor, 1.3 cal stability, simulated apogee 895 m and max velocity 191 m/s.
Pl. 3The Tier D trainer, a purple rocket with a blue nose cone, on the rail of a red launch pad on artificial turf.
Pl. 4The Tier D trainer after recovery, lying on turf with its blue nose cone and black plastic parachute still tethered.
Pl. 5A hand-laid fiberglass body tube standing upright on a digital kitchen scale.
Pl. 6Layup setup: woven fiberglass cloth on plastic sheeting with a film-wrapped steel-pipe mandrel, plus scissors, gloves, stir sticks and resin hardener.
Pl. 7CAD render of the Tier F rocket with a see-through body tube showing the motor mount, centering rings and an internal payload, with CG/CP markers and swept fins.
Pl. 8OpenRocket vertical motion vs. time: altitude peaks near 2,920 ft at about 12 s, acceleration runs about 500 ft/s² during the burn, and spikes at recovery deployment near 14.8 s.
Pl. 9Four team members pose with the silver, gold-nosed rocket in a lab with rocket airframes hung from the ceiling.
Pl. 10The silver airframe held up outdoors, signed "Henry, Sam, Jason, Justin", with its gold nose cone and swept fins.
Pl. 11The silver rocket with an orange nose cone and "Team Team" written on the body, on a launch rail at pad C.
5.0

Anomaly report

Closed
Observed
Air bubbles in the first fiberglass layup.
Corrective action
Cut the tube and kept only the section with the best structural quality.
Lesson
Concentricity came from the steel mandrel. Quality came from being willing to throw material away.