Model Rocket Design Notes
Dimensions
Engines
Type | | Diameter | Length | Casing |
MicroMaxx | | 6.3mm | 26mm | 1mm |
Mini | | 13mm | 45mm | 1.6mm |
18mm | | 18mm | 70mm | 2.6mm |
Tube | | Inside Dim. | Outside Dim. | Length |
| | mm/in | mm/in | cm/in |
MM Stand | | 4.00 / 0.157 | 4.50 / 0.177 | 1.35 / 0.53 |
Body Tubes
Tube | | Inside Dim. | Outside Dim. | Wall | Circumference | | Estes OD | ASP OD |
| | mm/in | mm/in | mm/in | mm/in | | | |
T-MM | | 6.45 / 0.254 | 7.16 / 0.282 | 0.355 | 22.49 / 0.886 | | | 7.1 |
T-10.5 | | 10.72 / 0.422 | 11.38 / 0.448 | | 35.75 / 1.41 |
BT-5 | | 13.2 / 0.518 | 13.8 / 0.544 | | 43.35 / 1.707 | | 13.7 | 13.7 |
BT-20 | | 18.0 / 0.710 | 18.7 / 0.736 | | 58.75 / 2.313 | |
BT-50 | | 24.1 / 0.950 | 24.8 / 0.976 | | 77.91 / 3.064 | |
BT-55 | | 32.6 / 1.283 | 33.7 / 1.325 | | 105.87 / 4.168 | |
BT-56 | | 33.1 / 1.304 | 34.2 / 1.346 | | 107.44 / 4.230 | |
BT-60 | | 40.5 / 1.595 | 41.6 / 1.637 | | 130.69 / 5.145 | |
BT-80 | | 65.7 / 2.588 | 66.0 / 2.600 | | 207.35 / 8.163 | |
Scaling
Src | | Dst | | Ratio |
BT-5 | | T-MM | | 51.88% |
| | BT-60 | | 300% |
BT-20 | | T-MM | | 38.29% |
| | BT-5 | | 73.8% |
Limits
Ground Hit Speed
"From how high would I be comfortable just dropping a rocket?"
Assuming a standing start and no air resistance yields freefall numbers like:
30mph | | 44fps | | 30.1' |
23.86mph | | 35fps | | 19.0' | | Tripoli safety code limit |
17.05mph | | 25fps | | 9.7' |
15.00mph | | 22fps | | 7.5' |
13.63mph | | 20fps | | 6.2' |
10.23mph | | 15fps | | 3.5' |
6.82mph | | 10fps | | 1.5' |
Electronics
Jolly Logic Altimeter Two
- 49mm x 18mm x 14.5mm (diameter 23.114mm)
- 9.9g (0.35oz)
Stability Notes
Velocity off rod should generally be at least 15 m/s (very rough rule of thumb).
Stability (CP-CG) should be 1--2 caliber for "normal" rockets.
- "Normal" here is fineness at/above 10:1.
Base drag of stubby rockets requires special attention
- "Stubby" is more or less rockets with fineness below 10:1
- OpenRocket accounts for base drag in its simulation, but not in calculation of CP for stability
- To account for this, add a 0g cone at the end of the rocket with fore diameter 0mm, aft diameter same as the body tube, and length π*diameter
- Discussion in Apogee Newsletter 154
Component Notes
Nosecones
Nosecone plug length should be approximately the diameter of the tube.
Couplers
Coupler construction video from Apogee.
Tube couplers should be ~2x the diameter of the tube.
Fins
Orient grain of balsa wood along leading edge of fins.
Engine Retention
Minimum diameter engine hook
There's a motor retention technique for minimum diameter rockets shown in Tim van Milligan's book that uses a piece of piano wire bent into three sides of a rectangle, two long sides and one short, where the short side goes over part of the bottom of the engine, staying clear of the nozzle of course, and the long sides are buried in fin fillets. I've started using that method on larger than minimum diameter rockets, with the ling sides going through pinholes in the aft centering ring. It seems like that should work nicely for MicroMaxx.
Recovery Systems
Ejection Baffles
Apogee Newsletter 129: Ejection Baffles
Parachutes
Parallel shrouds may prevent tangling:
Paper parachute wrapper
Links
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Scale Data
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