Skyreach
A 2018 N-class design for the 30,000 ft category.
- Stages
- Single-stage
- Propulsion
- Solid
- Motor
- Cesaroni Pro98 N3301
- Length
- 2.68 m
- Diameter
- 130 mm
- Apogee
- 30,000 ft target
Skyreach was ARD's 2018 design for the 30,000 ft category of the 2019 Australian Universities Rocket Competition, as Team 7: a 268 cm rocket, 13 cm in diameter, on a Cesaroni Pro98 N3301, simulated to 30,322 ft at Mach 1.87. Its recovery plan called for CO2 ejection, the idea Project Kronos brought back as its primary system.
01Anatomy
Take it apart
C-01·Nose cone
Nose cone
C-02·Avionics bay
Avionics bay
RRC3 and Raven 3 flight computers.
- Flight computers
- RRC3, Raven 3
C-03·Recovery system (parachutes)
Recovery system
A 3 ft drogue, then a 16 ft main at about 2,000 ft, with CO2 ejection.
- Drogue
- 3 ft
- Main
- 16 ft, at about 2,000 ft
- Ejection
- CO2
C-04·Motor and propulsion
Motor section
A 98 mm Cesaroni Pro98 N3301.
- Motor
- Cesaroni Pro98 N3301 (N class)
- Total impulse
- 19,317.6 N·s
- Average thrust
- 3,294.3 N
- Burn time
- 5.86 s
C-05·Fin can
Fin can
02Systems
Propulsion and ground
Stage 1 · Motor
Cesaroni Pro98 N3301
- Propellant
- Solid
- Impulse class
- N
Total impulse 19,317.6 N·s, average thrust 3,294.3 N, burn time 5.86 s.
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