Afstand
Kies de afstandseenheid: Meter(m), Voet(ft), Mijl(mi) of Kilometer(km)
Snelheid
Kies de snelheidseenheid: m/s, ft/s, mph of km/h
Versnelling
Kies de versnellingseenheid: m/s² of G
Vlucht 2788

Flight 2788

Nano V1 Rev 4 · firmware 1.61Secure 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.
Apogeum
103.6m
4.59 s after launch
Max. stijging
158.37m/s
peak ascent
Max. tijdens verbranding
9.3G
during the burn
Landing
0s
touchdown 0.03 m/s
ZOOM TO
s
s
Toon gebeurtenissen
Temp. & druk aanpassen ?
Afbeelding
Zoom
Klik en sleep, of knijp op mobiel
Vlucht vergelijken ?
Vluchtsamenvatting

The flight, moment by moment

Liftoff
0 s
Helling lanceerplatform82.30°
Thrust calc pad tilt10.5°
Landing
0 s
Hoogte-0.01 m
Max. daling-29.04 m/s
Launch detected
1.037 s
Hoogte30 m
Snelheid43.79 m/s
Uitbranding (eerste)
1.08 s
Hoogte31.51 m
Snelheid41.280 m/s
Apogeum
4.59 s
Hoogte103.6 Meter
Max. helling tot uitbranding140.66°
Mogelijke uitwerping
4.755 s
Hoogte58.42 m
Snelheid-0.73 m/s

Stabiliteit61%Matig

Helling bij burnout (20%)73.6
20% · Launch tilt 10.5°
Stamp/gier snelheid (30%)73.1
25% · Coning 60.6/50.2°/s
Coning · boost (25%)79.8
25% · Spin 151.2°/s
Stuwkrachtrechtheid (15%)26.9
30% · Thrust 83.9%

Rocket information

Calculated from the flight data alone
Boost acceleration38.2 m/s²
average over the burn · 3.9 g
Coast deceleration11.8 m/s²
average · gravity plus drag
Ballistic coefficient173 kg/m²
fitted to the 3.51 s coast
Apogee lost to tilt1.73 m
flown vertical ≈ 105.3 m · from the thrust-calculated tilt
Chute opening peak44.69 G
largest deceleration after ejection
Batterij & temperatuur 73% → 70% · Temperatuur start 32.17 → 32.33 °C · Lancering na inschakelen 1m 9s

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.

Helling bij burnout (20%)20%How close to vertical it left the rod.
Stamp/gier snelheid (30%)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.
Stuwkrachtrechtheid (15%)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.

Hoogte
Apogeum103.6 Meter
Tijd tot apogeum4.59 s
Hoogte uitbranding31.51 m
Hoogte max. snelheid89.83 m
Hoogte uitwerping58.42 m
Hoogte landing-0.01 m
Opnamehoogte26.07 m
Snelheid
Max. stijging158.37 m/s
Max. daling-29.04 m/s
Bij uitbranding41.280 m/s
Snelheid daling-3.897 m/s
Snelheid uitwerping-0.73 m/s
Snelheid landing0.032 m/s
Versnelling
Max. tijdens verbranding9.3 G
Max. stijging9.3 G
Max. daling44.69 G
Gem. stijging0.48 G
Gem. verbranding4 G
Tijden
Uitbranding (eerste)1.08 s
Apogeum4.59 s
Mogelijke uitwerping4.755 s
Landing0 s
Hoeken
Helling lanceerplatform82.30°
Thrust calc pad tilt10.5°
Max. helling tot uitbranding140.66°
Rol bij lancering77.25°
Stamp bij lancering-52.41°
Max. rotatie (verbr.)1800.44 dps
Gem. rotatie (verbr.)291.95 dps
Staging
Stages detected5
Stage S1 burnout
flip1.037 s
drag1.204 s
sig1.188 s
Stage S2 ignition3.632 s
Stage S2 burnout
flip3.761 s
Stage S3 ignition3.632 s
Stage S3 burnout
flip3.761 s
Stage S4 ignition3.632 s
Stage S4 burnout
flip3.761 s
Stage S5 ignition3.632 s
Stage S5 burnout
flip3.761 s
drag3.791 s
sig3.931 s
Recovery
Single deploy
No dual deploy detected on this flight.
Algemeen
Uploaddatum14/08/26-15:13:03
Datapunten6700
Totale opnametijd41.945 s
Gem. monsters/s159.7
Aantal vergrendelingen0
Lancering na inschakelen1m 9s
Referentie-asY
Batterij & temperatuur
Batterij start73%
Batterij einde70%
Temperatuur start32.17°C
Temperatuur einde32.33°C
Gebruikersnotities
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Youtube-video
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Vluchtafbeeldingen 0
Geen afbeeldingen
Vluchtmotoren
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Gekoppelde raket
Geen raket gekoppeld aan deze vlucht

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.

!The altimeters aboard disagree on apogee by 34.6%
Apogee spread67.8 – 103.6 m
#2895 · Nano V1Same flight · another altimeter67.8 mView flight →

Lanceerplaats, datum & tijd

Klik op de kaart om uw lanceerlocatie te markeren. Schakel tussen kaart- en satellietweergave.

Imagery © Esri, Maxar, Earthstar Geographics

Klik op de kaart · Sleep om aan te passen

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.

Vluchtdata-animatie

FLIGHT 2788

103.6 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

Opmerking: De vluchtanimatie vereist dat uw hoogtemeter in een vaste oriëntatie is gemonteerd. Kalibreer uw sensoren voor de beste resultaten.
Nano V1
Revision 4
Nano V1
Deze vlucht is gevlogen met een Nano V1.
The hardware
HardwareversieRev 4
Softwareversie1.61
Laatst online14/08/26-15:13:03
DruksensorBosch BMP 581
Versnellingsmeter32G 3-axis
Gyroscoop2000 dgps 3-axis

Settings, as they were for this flight

Algemene vluchtinstellingen
Voorspelde druk
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
Lanceerdetectie
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 (400Hz)
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.
400 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.
INGESCHAKELD (45 samples / 111.97ms)
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
Sensorkalibratie
Kalibratie-offsets gebruikt voor deze vlucht.
Gyroscoop
X2.000°
Y0.000°
Z0.000°
Versnellingsmeter⚠ Versnellingsmeter is niet gekalibreerd
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
2788.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
645 KB
LOG
2788.aclz ✓ SIGNED
The altimeter's own compressed log, exactly as the device wrote it. This is the file to keep for a record claim.
93 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.

Vlucht
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