In development2025

Two-Stage L2

ARD's first two-stage design: a Level 2 rocket at simulation stage.

Stages
Two-stage
Propulsion
Solid
Motor
AeroTech HP-J270W / Cesaroni 315H255-14A
Length
1.6 m
Diameter
86.6 mm

A two-stage Level 2 rocket designed in OpenRocket: a sustainer on a Cesaroni 315H255-14A, boosted by an AeroTech HP-J270W. Each stage has four carbon-fibre fins and its own parachute. The design is at simulation stage.

01Anatomy

Take it apart

Scroll to separate the rocket into its components. Each one is explained as it comes into view.

C-01·Nose cone · Stage 2 (sustainer)

Nose cone

A parabolic fibreglass nose cone.

Shape
Parabolic
Material
Fibreglass
Length
300 mm

C-02·Recovery system (parachutes) · Stage 2 (sustainer)

Sustainer recovery

The sustainer's parachute, deployed at apogee.

Parachute
68.5 cm, at apogee

Technology · Recovery lineage

C-03·Motor and propulsion · Stage 2 (sustainer)

Sustainer motor

A 29 mm Cesaroni 315H255-14A in the aft end of the 700 mm sustainer tube.

Motor
Cesaroni 315H255-14A (29 mm, H class)
Body tube
700 mm fibreglass

C-04·Fin can · Stage 2 (sustainer)

Sustainer fins

Four freeform carbon-fibre fins.

Count
4
Material
Carbon fibre

C-05·Interstage · Stage 1 (booster)

Interstage

A 160 mm coupler joins the booster to the sustainer.

Coupler
160 mm

C-06·Recovery system (parachutes) · Stage 1 (booster)

Booster recovery

The booster's own parachute, deployed at 200 m on the way down.

Parachute
65 cm, at 200 m

Technology · Recovery lineage

C-07·Motor and propulsion · Stage 1 (booster)

Booster motor

A 38 mm AeroTech HP-J270W in the 600 mm booster tube.

Motor
AeroTech HP-J270W (38 mm, J class)
Body tube
600 mm fibreglass

C-08·Fin can · Stage 1 (booster)

Booster fins

Four freeform carbon-fibre fins.

Count
4
Material
Carbon fibre

02Systems

Propulsion and ground

Stage 1 · Motor

AeroTech HP-J270W

Propellant
Solid
Impulse class
J

Booster motor, 38 mm.

Stage 2 · Motor

Cesaroni 315H255-14A

Propellant
Solid
Impulse class
H

Sustainer motor, 29 mm.

Side-on CAD section view of a two-fin-set rocket with colour-coded internal sections: green nose cone, red forward fins and blue aft fins.
Two-stage L2 rocket CAD, 2025.

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