Altimeter Bay Design Calculator
Design your rocket's avionics bay. Calculate internal volume, verify component fit, and size vent holes for accurate barometric altitude readings.
About this calculator
An altimeter bay (also called an avionics bay or e-bay) is the section of a dual-deploy high-power rocket that holds the flight computer, battery, and black-powder ejection charges, with vent holes drilled through the coupler so the barometric sensor reads true ambient pressure. This calculator sizes that bay from your airframe's body tube dimensions and the electronics you plan to mount. Bay volume is driven mainly by body tube outer diameter -- diameter enters the cross-sectional area as a squared radius term, so it moves calculated volume more than a proportional change in bay length does, with wall thickness making only a small further reduction. The usable inner diameter subtracts twice the wall thickness from the outer diameter, since the wall exists on both sides of the bore.
Vent hole area scales with hole diameter as a squared term per hole, and total open area also scales in direct proportion with how many holes you drill at that diameter -- doubling the hole count doubles total vent area just as surely as doubling the area of a single hole does. The pressure equalization time constant balances two competing effects: a larger bay volume takes longer to equalize (increasing the time constant), while larger vent holes equalize faster (decreasing it) -- these two effects are close enough in magnitude at the shipped defaults that neither one dominates decisively. Electronics boards are assumed to mount lengthwise on a sled inside the tube, so only the board's WIDTH is checked against the inner diameter; its length is budgeted separately against total bay length, alongside black-powder canisters and wiring clearance. This calculator does not model sled rail thickness, bulkhead hardware, or U-bolt clearance, all of which consume real usable length beyond what is estimated here -- treat the remaining-length output as a rough margin check, not a final go/no-go.
Inputs
Results
Bay volume (cc)
405.4
How to Use This Calculator
- Enter Body tube OD (mm), Wall thickness (mm), and Bay length (mm).
- Set Altimeter board length (mm), Altimeter board width (mm), and Battery length (mm).
- Adjust Battery diameter (mm), Number of vent holes as needed.
- Review the Bay volume (cc) result.
- Use Inner diameter (mm) and Total vent area (mm²) to inform your decision.
How the result changes with Body tube OD (mm)
| Body tube OD (mm) | Bay volume (cc) |
|---|---|
| 27 | 89 |
| 41 | 224.4 |
| 81 | 950.8 |
| 135 | 2,728.7 |
What each input means
- Body tube OD (mm)
- Outside diameter of the avionics bay tube.
- Wall thickness (mm)
- Tube wall thickness. Typical: 1.5-2mm for phenolic, 0.8-1.2mm for fiberglass.
- Bay length (mm)
- Internal length available for electronics between bulkheads.
- Altimeter board length (mm)
- Length of your altimeter PCB. StratoLoggerCF: 50mm, Featherweight Raven3: 65mm.
- Altimeter board width (mm)
- Width of your altimeter PCB.
- Battery length (mm)
- Length of the flight battery (typically 9V or LiPo).
- Battery diameter (mm)
- Diameter or width of the flight battery.
- Number of vent holes
- Number of vent holes in the bay coupler. Minimum 3 recommended, evenly spaced.
- Vent hole diameter (mm)
- Diameter of each vent hole. 1/4 inch (6.35mm) is a common minimum.
What each result means
- Bay volume (cc)
- Internal volume of the avionics bay.
- Inner diameter (mm)
- Usable inner diameter after accounting for wall thickness.
- Total vent area (mm²)
- Combined open area of all vent holes.
- Pressure time constant (ms)
- How quickly internal pressure equalizes. Should be well under 100ms.
- Component stack length (mm)
- Estimated total length of altimeter + battery + BP canisters + wiring.
- Remaining length (mm)
- Spare room in the bay after components. Positive = fits.
- Recommended vent holes
- Minimum recommended number of vent holes for this bay volume.
How this is calculated
Worked example, using the default values
- Identify Input Parameters9 parametersBody tube OD (mm) = 54, Wall thickness (mm) = 1.6, Bay length (mm) = 200, Altimeter board length (mm) = 65, Altimeter board width (mm) = 20, Battery length (mm) = 50, Battery diameter (mm) = 14, Number of vent holes = 3, Vent hole diameter (mm) = 6.35 = 9 input(s) provided
- Calculate Bay volumeBay volume = π * (innerRadiusMm / 10) ^ 2 * (bayLengthMm / 10)405.4 = 405.4
- Calculate Inner diameterInner diameter = bodyDiameterMm - 2 * wallThicknessMm50.8 = 50.8
- Calculate Total vent areaTotal vent area = numVentHoles * singleHoleAreaMm295 = 95
Engine last updated . Checked against 2 independently-derived tests — how we verify calculators. Built by Paul Gunder, a software engineer, not a licensed financial, medical, or legal professional.
Frequently Asked Questions
Why does body diameter affect bay volume more than bay length does?
Volume follows pi x radius-squared x length: diameter enters as a squared radius term while length enters linearly, so a given percentage increase in diameter compounds through the square and moves total volume more than the same percentage increase in length, at this calculator's default dimensions.
Does adding more vent holes increase the total vent area?
Yes -- total vent area is each hole's area (from its diameter) multiplied by how many holes you specify, so adding holes at a fixed diameter increases total open area in direct proportion. Drilling a fourth hole the same size as your first three adds another equal share of open area, exactly like adding a fourth equal-sized window to a wall.
How much spare room should I leave beyond the calculated remaining length?
The remaining-length output only budgets the altimeter board, battery, black-powder canisters, and a fixed wiring clearance -- it does not account for sled rail thickness, bulkhead hardware, or U-bolt clearance, all of which consume real length inside the bay. Treat a small positive remaining length as tight, not comfortable, and aim for at least 10-20mm of additional margin beyond what this calculator reports before you commit to a coupler length.
Why is the fit check based on the altimeter board's width instead of its diagonal?
Avionics boards mount on a sled that slides in along the tube's length, so the board's LENGTH runs parallel to the tube axis and is already accounted for in the bay's total length budget -- only the board's WIDTH crosses the circular bore and needs to clear the inner diameter. Checking the board's diagonal would incorrectly assume it is mounted crosswise, which would reject boards that actually fit fine on a standard sled.
What is the pressure time constant, and why doesn't one input clearly dominate it?
It estimates how quickly air pressure inside the bay equalizes with the outside through the vent holes, based on bay volume divided by vent area and the speed of sound. A larger bay volume slows equalization while larger vent holes speed it up, and at this calculator's default dimensions those two competing effects are close enough in size that neither one moves the result decisively more than the other.
Related Calculators
The questions that sit next to this one — chosen by subject, including calculators filed under a different category.
Dual Deploy Calculator
Size drogue and main parachutes for dual-deployment recovery. Calculates chute diameters, descent times, opening shock, and black powder ejection charges.
Amateur RocketryRecovery System Calculator
Size your rocket parachute for a safe descent rate. Calculates canopy diameter, area, landing energy, and drift distance using aerodynamic drag equations.
Amateur RocketryFin Flutter Speed Calculator
Calculate the critical flutter velocity for rocket fins based on material shear modulus, fin geometry, and altitude using the NARTS approximation.
More in Science & Physics.