Distance
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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)
Flight 1359

Flight 1359

Nano V1 Rev 4 · firmware 1.50
Apogee
135.6m
5.56 s after launch
Max ascent
48.41m/s
peak ascent
Max during burn
6.69G
during the burn
Landing
32.72s
touchdown 5.24 m/s
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Flight summary

The flight, moment by moment

Liftoff
0 s
Launch pad tilt97.89°
Thrust calc pad tilt13.5°
Launch detected
0.929 s
Altitude25.05 m
Velocity39.06 m/s
Burnout (first)
1.66 s
Altitude58.82 m
Velocity44.320 m/s
Apogee
5.55 s
Altitude135.6 Meters
Max tilt to burnout119.41°
Possible ejection
6.332 s
i
This ejection time was detected by the website from the accelerometer data, because the firmware did not record one for this flight.
Altitude132.15 m
Velocity-7.21 m/s
Landing
32.72 s
Altitude-2.32 m
Max descent-12.04 m/s

Stability89.4%Excellent

Launch straightness (20%)66.1
20% · Launch tilt 13.5°
Coning · full (25%)97.9
25% · Coning 14.5/19.1°/s
Coning · boost (25%)96.4
25% · Spin 64.1°/s
Thrust straightness (30%)91.9
30% · Thrust 98.4%

Rocket information

Calculated from the flight data alone
Boost acceleration26.7 m/s²
average over the burn · 2.7 g
Coast deceleration11.4 m/s²
average · gravity plus drag
Ballistic coefficient134 kg/m²
fitted to the 3.89 s coast
Apogee lost to tilt3.74 m
flown vertical ≈ 139.3 m · from the thrust-calculated tilt
Chute opening peak20.95 G
largest deceleration after ejection
Average descent rate5.09 m/s
ejection to landing · 26.39 s
Battery & temperature 96% → 96% · Temperature start 16.45 → 16.2 °C · Launch after startup 1m 52s

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
Apogee135.6 Meters
Time to apogee5.55 s
Burnout altitude58.82 m
Max velocity altitude44.67 m
Ejection altitude132.15 m
Landing altitude-2.32 m
Recording altitude37.61 m
Velocity
Max ascent48.41 m/s
Max descent-12.04 m/s
At burnout44.320 m/s
Descent velocity-5.076 m/s
Ejection velocity-7.21 m/s
Landing velocity-5.243 m/s
Acceleration
Max during burn6.69 G
Max ascent6.69 G
Max descent20.95 G
Average ascent0.28 G
Average burn2.49 G
Times
Burnout (first)1.66 s
Apogee5.55 s
Possible ejection6.332 s
Landing32.72 s
Angles
Launch pad tilt97.89°
Thrust calc pad tilt13.5°
Max tilt to burnout119.41°
Launch roll99.13°
Launch pitch-30.15°
Max spin (burn)204.8 dps
Avg spin (burn)69.47 dps
Recovery
Single deploy
No dual deploy detected on this flight.
General
Upload date09/04/26-01:31:51
Data samples4294
Total recording time45.107 s
Average samples/s95.1
Number of lockouts0
Launch after startup1m 52s
Reference axisY
Battery & temperature
Battery start96%
Battery end96%
Temperature start16.45°C
Temperature end16.2°C
User notes
No notes added
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Youtube video
No video added
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Flight images 0
No images added
Flight motors
1st stage · 5s delay
1×C6-5KlimaDetails
Burn time
1.6 s
Diameter
18.00 mm
Average thrust
6 N
Max thrust
15 N
Total weight
20.50 g
Propellant weight
9.60 g
Propellant type
composite
Impulse10Ns
Max thrust15N
Burn time1.6s
Impulse classC
1st stage thrustloading curve…
Motor data by ThrustCurve.org
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Linked rocket
No rocket linked to this flight
Flight mass
Liftoff mass140.1gestimated
Mass at burnout130.5gestimated
No mass is set for this flight, so Motor thrust (N) uses a mass estimated from the measured burn and the motors’ rated impulse. Set the rocket’s mass for the measured impulse and specific impulse.
Motor thrust (N) is on the chart, under Acceleration.

Linked flights

Connect flights that belong together: a second altimeter flown in the same rocket, or the same rocket flown again. Linked flights appear on each other’s pages.

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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.

No launch site has been set for this flight.

Flight data animation

FLIGHT 1359

135.6 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
Revision 4
Nano V1
This flight was flown on a Nano V1.
The hardware
Hardware versionRev 4
Software version1.50
Last online09/04/26-01:31:51
Pressure sensorBosch BMP 581
Accelerometer32G 3-axis
Gyroscope2000 dgps 3-axis

Flights from this altimeter

6 of 6

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.
25 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 (100Hz)
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.
24000
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.
100 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.
Disabled
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 (39 samples / 395ms)
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.
Down (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.
Madgwick 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.
1.5G
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
X0.082°
Y1.044°
Z0.057°
Accelerometer
X224.710 mG
Y4.850 mG
Z14.470 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
1359.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
325 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.
Data sets
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.

Flight
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