Distance
You can choose which units to use for distance from Meters(m), Feet(ft), Miles(mi) & Kilometers(km)
Velocity
You can pick which units to use for Velocity/speed such as Meters per second (m/s), Feet per second (ft/s), Miles per hour (mph) and Kilometers per hour (kph)
Acceleration
You can choose acceleration units to display from either Meters per second squared (m/s^2) or Gravity (G)

Chiefs BB flight 50

Nano V1 Rev 4 · firmware 2.00Secure logSecure logThe altimeter signed this log and it passed verification on upload, so the data is unchanged since the device wrote it.Signatures use Ed25519, which no current technology can forge.
Apogee
199.24m
6.39 s after launch
Max ascent
86.11m/s
peak ascent
Max during burn
16.97G
during the burn
Landing
66.02s
touchdown 4.74 m/s
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Flight summary

The flight, moment by moment

Liftoff
0 s
Rail angle6.9°
Rail kick19.94°
Burnout (first)
0.7 s
Altitude0 m
Velocity86.110 m/s
Launch detected
0.70402 s
Altitude30.15 m
Velocity86.11 m/s
Possible ejection
5.727 s
Altitude0 m
Velocity m/s
Apogee
6.39 s
Altitude199.24 Meters
Max tilt to burnout18.51°
Landing
66.01 s
Altitude0 m
Max descent-5.33 m/s

Stability74.1%Good

Launch straightness (20%)82.5
20% · Rail angle 6.9°
Coning · full (25%)84.5
25% · Coning 42.7/77.9°/s
Coning · boost (25%)62.1
25% · Spin 307°/s
Thrust straightness (30%)69.9
30% · Thrust 93.5%

Rocket information

Calculated from the flight data alone
Boost acceleration123.0 m/s²
average over the burn · 12.5 g
Coast deceleration15.1 m/s²
average · gravity plus drag
Ballistic coefficient172 kg/m²
fitted to the 5.69 s coast
Apogee lost to tilt3.63 m
flown vertical ≈ 202.8 m · from the tilt at burnout
Chute opening peak49.82 G
largest deceleration after ejection
Battery & temperature 62% → 60% · Temperature start 40.02 → 38.9 °C · Launch after startup 46m 6s

About the stability score

Worked out from the flight log between liftoff and 80% of apogee. It is independent of the angle the altimeter was mounted at, so it measures the flight rather than the fitting.

Launch straightness (20%)20%How close to vertical it left the rod.
Coning · full (25%)25%How much the nose swung off the rocket's own axis across the whole ascent.
Coning · boost (25%)25%The same swing during the burn, when it matters most.
Thrust straightness (30%)30%How cleanly the motor pushed along the body.

Spin about the rocket's own axis is not counted against it — a fast, straight spin is stable. The figures beside the score are the raw measurements behind these four.

Altitude
Apogee199.24 Meters
Time to apogee6.39 s
Burnout altitude0 m
Max velocity altitude30.59 m
Ejection altitude0 m
Landing altitude0 m
Recording altitude1302.54 m
Velocity
Max ascent86.11 m/s
Max descent-5.33 m/s
At burnout86.110 m/s
Descent velocity-3.321 m/s
Ejection velocity m/s
Landing velocity-4.735 m/s
Acceleration
Max during burn16.97 G
Max ascent43.88 G
Max descent49.82 G
Average ascent2.08 G
Average burn12.88 G
Times
Burnout (first)0.7 s
Apogee6.39 s
Possible ejection5.727 s
Landing66.01 s
Angles
Rail angle ?6.9° ± 0.5°
Rail kick ?19.9°
Max tilt to burnout ?18.51°
Orientation ?97.52°
Mount offset ?100.7° orientation setting looks wrong
Launch roll-99.47°
Launch pitch37.30°
Max spin (burn)465.12 dps
Avg spin (burn)232.38 dps
Staging
Stages detected1
Burnout (refined)0.739 s
Stage S1 burnout
flip0.704 s
drag0.744 s
sig0.854 s
Recovery
Single deploy
No dual deploy detected on this flight.
General
Upload date26/10/26-01:26:24
Data samples11490
Total recording time79.446 s
Average samples/s144.6
Number of lockouts0
Launch after startup46m 6s
Reference axisX
Battery & temperature
Battery start62%
Battery end60%
Temperature start40.02°C
Temperature end38.9°C
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User notes
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Youtube video
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Flight images 0
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Flown as
Rocket
Estes Industries
Motor configuration
Custom
1× Quest C12-4, set on this flight
Loaded weight
106.8 g
set on this flight · estimated 98.6 g from the rated impulse

Measured burn

from this flight’s thrust and its loaded weight
Total impulse, NFPA 112510.67 Ns
rated 9.80 Ns, 8.9% over, within the 20% NFPA 1125 allows
Total impulse, absolute10.67 Ns
Measured asD15
sold as a C12
Burn time, NFPA 11250.73 s
0.00 to 0.73 s
Average thrust14.7 N
impulse over burn time
Peak thrust19.6 N
at 0.60 s
Specific impulse105 s
10.4 g of propellant
Mass at burnout96.4 g
loaded weight less propellant
NFPA 1125, the code motors are certified to by NAR, Tripoli and CAR: the burn runs from where the thrust first rises above 5% of its peak to where it falls below it (7.8.3), and the total impulse from that rise to the last measurable thrust before ejection (7.8.5). Absolute counts every newton from liftoff. The same code lets a production lot vary 20% from its mean impulse for a model rocket motor and 10% for high power (7.8.6). Both figures follow the loaded weight: 1% out on the weight is about 1% out on the impulse. Here the thrust passed 5% of its peak before liftoff, while the pad held the rocket, so the NFPA 1125 figures start at liftoff.
Flight motors
1st stage · 4s delay
1×C12-4QuestDetails
Burn time
0.84 s
Diameter
18.00 mm
Average thrust
11.7 N
Max thrust
17.5 N
Total weight
23.70 g
Propellant weight
10.40 g
Propellant type
Black Max
Impulse9.8Ns
Max thrust17.5N
Burn time0.84s
Impulse classC
1st stage thrustloading curve…
Motor data by ThrustCurve.org
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Linked rocket
🚀
Active
Chiefs Big Bertha
Estes Industries — Big Bertha
1 flight linked
Type
Kit build
Diameter
66.7mm
Length
685.8mm
Empty weight
79.1g
Stages
1
Fins
4
Recovery
Parachute
Chute
31cm
Body
Kraft Paper
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Launch site, date & time

Click anywhere on the map to mark your launch site. Switch between map and satellite view using the buttons below.

Imagery © Esri, Maxar, Earthstar Geographics

Click the map to place a marker · Drag to adjust

Canopy height from the Meta and WRI High Resolution Canopy Height Maps v2 (Meta and World Resources Institute, 2026; source imagery © 2016 Vantor), used under CC BY 4.0. Ground elevation built from Terrain Tiles (Mapzen and AWS Open Data), derived from 3DEP and GMTED courtesy of the U.S. Geological Survey, SRTM courtesy of NASA, and ETOPO1 courtesy of NOAA. Map and imagery credited on the view above.

Site namePlayas Training Center - NSL WestLat31.943667Lng-108.548579Ground level1350.8 m · 4432 ftLaunch date2026-10-25Launch time16:00
Flight data animation

FLIGHT 3166

199.24 Meters

ALTITUDE
0.00m
VELOCITY
0.00m/s
ACCEL
0.00G
TILT
0.00°
PITCH
0.00°
ROLL
0.00°
YAW
0.00°
TIME
0.00s
AWAITING LAUNCH
ALT
altimetercloud.com
LAUNCH T+0.00s LANDING

BURNOUT

Motor burn complete

Note: Flight profile animation requires your altimeter to be mounted in a fixed orientation that you choose in your settings. For best results please calibrate your sensors as well.
Nano V1
Rocketry Ltd

Nano V1

Compact altimeter for small rockets. This flight was flown on a Nano V1.
Hardware version Rev 4Software version 2.00Last online 26/10/26-01:26:24

Specifications

Electronics

Microcontroller
ESP32-S232-bit ESP32-S2 240MHz
Accelerometer
ST LSM6DSO3232G 3-axis (SPI)
Barometer
Bosch BMP581300 to 1250 hPa within specification
Gyroscope
ST LSM6DSO322000 dgps 3-axis

Logging

Maximum sample rate
833 Hz
Most samples in a log
38,000
Longest log
1 h 3 minAt 10Hz although default settings are 433Hz with 1:8 hybrid mode

Electronics

Microcontroller
ESP32-S232-bit ESP32-S2 240MHz
Accelerometer
ST LSM6DSO3232G 3-axis (I2C)
Barometer
Bosch BMP581300 to 1250 hPa within specification
Gyroscope
ST LSM6DSO322000 dgps 3-axis

Logging

Maximum sample rate
833 Hz
Most samples in a log
38,000
Longest log
1 h 3 minAt 10Hz although default settings are 433Hz with 1:8 hybrid mode

Size, weight and battery

Size
20 × 10 × 8.9 mm
Weight
1.65 g1.65 g with the smallest battery
Battery voltage
3 to 4.2 V
Battery life
5on the smallest battery
Size
20 × 10 × 8.9 mm
Weight
1.65 g1.65 g with the smallest battery
Battery voltage
3 to 4.2 V
Battery life
5on the smallest battery

Documents

Flights from this altimeter

20 of 3120 of 117

Settings, as they were for this flight

General flight settings
Forecast pressure
i
Set this to your local forecast pressure at sea level. This will offer you slightly improved accuracty for your flight, although it's not 100% essential every little helps!

Xcweather.co.uk is a decent place to grab pressures from for your location and time.
1013.2 mbar
Launch detect
i
This is the altitude above the launch pad altitude where the altimeter will trigger itself into recording / flight mode.

The altimeter keeps a constant average of the pressure while waiting for launch, it uses a simple algorithm and the pre-flight buffers to do this. The most recent 120 samples (~4 seconds) are ignored so your pre-trigger altitude won't effect the ground baseline.

For almost all uses we suggest keeping this on the 25 Meter (~82 feet) default settings. If you want to test your altimeter by throwing it in the air, or are planning a very low flight you may want to lower the setting.
30 meters
Sample ratio
i
The altimeter runs at 50Hz however you can record every sample or every X samples in order to extend the log time. For example if you set the ratio to 1 it will save 1:1 samples, or if you set it to 3 it will save 1 in 3 samples.
1:1:1 (417Hz)
Max samples
i
This is the maximum samples the altimeter will log per flight. When it reaches this amount it will stop and save the recording.
38000
Recording stop
i
This setting is how the altimeter decides to stop recording. You can choose either 450 (~9s) or 900 (~18s) samples stable or it will record until the max samples limit unless you press the BUTTON in Manual stop mode.

The samples stable method waits for the devices altitude not to change for the set number of samples. This is defined by not changing by more than +/- 1.0 meters for 98% of the samples, it's a reliable method to stop the recording after landing within 8-10 seconds (300 sample) or 16-20 seconds (600 sample).
Auto: 8s stable altitude
Oversampling
i
Oversampling is a internal setting of the BMP 390 pressure sensor. It is how many samples are taken for each reading. By taking multiple samples for each pressure reading the altimeter reduces noise and increases the resolution of the output.

The sensor can run at 50 samples per second in 4X mode, so we suggest leaving it in this mode as it will offer the highest accuracy.
16x Oversampling
IIR filter
i
The IIR filter is another internal sensor for the BMP390 pressure sensor. It is a Infinite impulse response filter used to enhance pressure measurement accuracy by reducing noise. It's primarily for smoothing out rapid pressure changes.

We suggest not setting this too high as it will cause delay to changes in altitude if set very high.
COEFF 7
Pressure filter
i
This filter is a software Kalman filter that runs on the altimeters processor.

The Kalman filter uses a prediction step based on a system model and then a correction step using new measurements to refine its estimate, it creates accurate most certain results from data with noise in it.
TruePath
Sample speed
i
The sample rate of the altimeter's sensors. 50Hz takes 50 samples per second, 100Hz takes 100 samples per second for higher resolution data.
417 Hz
Hybrid mode
i
When enabled, the altimeter records at full speed during ascent then switches to half speed after apogee to extend recording time during descent.
Enabled
Sync sensors
i
The filters on the pressure sensor can cause it to lag very slightly behind the Accelerometer and Gyroscope data. The Sync sensors option detects how far out of sync these sensors are. It then corrects the Acceleration and Gyroscope readings to match the pressure sensor.
ENABLED (44 samples / 109.42ms)
Orientation
i
This is the orientation you intend to install the Altimeter in your rocket. It's needed to ensure completly accurate angles and orientation charts and reports. Check out the Manual for more information on this.
On back (text up)
IMU filter
i
The IMU filter, or fusion filter takes the data from each axis of the Gyroscope and Accelerometer to calculate the Pitch, Roll, Yaw and tilt angle from vertical. These filters can build up some discrepency over time so it's important to calibrate your sensors to minimise this.
Attitude filter 6-Axis
Launch ALP
i
This is prevention against accidental launch detection.

With this disabled the launch is based only on pressure and something that creates a low pressure can trigger the flight by accident. For example pulling your nose cone off can even trigger it.

With this enabled the rocket also needs to have seen 8 samples (0.25 seconds) of acceleration above this setting in the last 3 seconds as well as the pressure drop to trigger. There is a backup trigger of 1.05 seconds of altitude being above the launch detect setting too.

There are very few situations where this option would cause issues, so we suggest leaving it on.
2.0G
Launch lock
i
When enabled, the altimeter locks out recording for a set period after power on to prevent false triggering during setup.
DISABLED
Static temperature
i
A fixed temperature value used for altitude calculation when the external temperature sensor is disabled or not connected.
15 °C
Sensor calibration
Calibration offsets used during this flight.
Gyroscope⚠ Gyroscope has not been calibrated
X0.000°
Y0.000°
Z0.000°
Accelerometer⚠ Accelerometer has not been calibrated
X0.000 mG
Y0.000 mG
Z0.000 mG

Files

Where the altimeter signs its log, the file carries that signature and a tick beside it. A tick means the data is unchanged since the device wrote it, which is what a record claim needs.
CSV
3166.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
1156 KB
LOG
3166.aclz ✓ SIGNED
The altimeter's own compressed log, exactly as the device wrote it. This is the file to keep for a record claim.
167 KB
WX
3166_weather.json.gz
The weather for 48 hours either side of the launch, within 15 km of the launch site: NOAA GFS every hour, at the surface and up to about 31 km, and the NOAA GEFS ensemble where this site holds it. JSON, gzip compressed. Weather data by Open-Meteo.com (CC BY 4.0) and NOAA. For 2026-10-25 16:00 local time at 31.9437, -108.5486.
1379 KB
Adjusted CSV2904 recalculated in your browser
The log recomputed for your own sea-level pressure and temperature. Columns: time, altitude as recorded and adjusted, raw altitude as recorded and adjusted, pressure.

This file is built here from the signed log, so it carries no signature of its own. Anyone verifying a claim should be sent to the flight page and build their own from the original.

Custom CSVbuilt in your browser
Pick any of the chart’s data sets, the worked-out ones included, and the part of the flight to cover. Values come in the units the chart is set to.
In the file
Time span

One row for every time any chosen data set has a sample. A data set with no sample at that time is left blank rather than filled in. Built from the chart’s data, so it carries no signature.

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