This document summarizes the specifications of a rocket designed with a single stage. It lists key flight parameters such as an altitude of 1368 meters, flight time of 107 seconds, and maximum velocity of 255 meters per second. The rocket utilizes a J330-16 motor with 375 grams of propellant that provides 765 Newton-seconds of total impulse.

1. Rocket Design
J330-16
Rocket
Stages: 1
Mass (with motor): 2445 g
Stability: 2.02 cal
CG: 104 cm
CP: 122 cm
Altitude 1368 m
Flight Time 107 s
Time to Apogee 14.6 s
Optimum Delay 12.4 s
Velocity off Pad 23.9 m/s
Max Velocity 255 m/s
Velocity at
Deployment
N/A
Landing Velocity 26.7 m/s
Motor Avg Thrust Burn Time Max Thrust Total Impulse Thrust to Wt Propellant Wt Size
J330 343 N 2.23 s 459 N 765 Ns 14.33:1 375 g 38/421
mm

2. Parts Detail
Sustainer
Nose cone Fiberglass
(1.85 g/cm³)
Conical Len: 45.7 cm Mass: 227 g
Body tube Fiberglass
(1.85 g/cm³)
Diain 8.49 cm
Diaout 8.89 cm
Len: 7.62 cm Mass: 77 g
Bulkhead Plywood (birch)
(0.63 g/cm³)
Diaout 8.49 cm Len: 0.635 cm Mass: 22.6 g
Tube coupler Fiberglass
(1.85 g/cm³)
Diain 8.09 cm
Diaout 8.49 cm
Len: 15.2 cm Mass: 147 g
Bulkhead Plywood (birch)
(0.63 g/cm³)
Diaout 8.09 cm Len: 0.635 cm Mass: 20.6 g
Body tube Fiberglass
(1.85 g/cm³)
Diain 8.49 cm
Diaout 8.89 cm
Len: 102 cm Mass: 1026 g
Inner Tube Fiberglass
(1.85 g/cm³)
Diain 3.8 cm
Diaout 4 cm
Len: 25.4 cm Mass: 57.6 g
Centering ring Plywood (birch)
(0.63 g/cm³)
Diain 4 cm
Diaout 8.49 cm
Len: 0.635 cm Mass: 17.6 g
Centering ring Plywood (birch)
(0.63 g/cm³)
Diain 4 cm
Diaout 8.49 cm
Len: 0.635 cm Mass: 17.6 g
Centering ring Cardboard
(0.68 g/cm³)
Diain 4 cm
Diaout 8.49 cm
Len: 0.635 cm Mass: 19 g
Trapezoidal fin set (4) Plywood (birch)
(0.63 g/cm³)
Thick: 0.318
cm
Mass: 67.9 g
Trapezoidal fin set (4) Plywood (birch)
(0.63 g/cm³)
Thick: 0.318
cm
Mass: 43.1 g

7. in cm
cm
in