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 2917

Flight 2917

Nano V1 Rev 3 · firmware 1.65Secure 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
320.61m
8.86 s after launch
Max. stijging
107.7m/s
peak ascent
Max. tijdens verbranding
0G
during the burn
Landing
45.72s
touchdown 6.34 m/s
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Toon gebeurtenissen
Temp. & druk aanpassen ?
Afbeelding
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Vluchtsamenvatting
Hoogte
Apogeum
320.61 Meter
Tijd tot apogeum
8.85 seconds
Snelheid
Max. stijging
107.69 m/s
Max. daling
-25.5 m/s
Tijden
Landing
45.71 seconds
Totale opnametijd
61.989 seconds
Gebruikersnotities
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Youtube-video
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Vluchtafbeeldingen 0
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Vluchtmotoren
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Gekoppelde raket
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Linked flights

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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

No launch site has been set for this flight.

Nano V1
Revision 3
Nano V1
Deze vlucht is gevlogen met een Nano V1.
The hardware
HardwareversieRev 3
Softwareversie1.65
Laatst online13/09/26-21:48:59
DruksensorBosch BMP 390

Flights from this altimeter

No other flights yet. This will fill up as you fly.

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 (50Hz)
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.
8x 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.
50 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
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

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
2917.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
126 KB
LOG
2917.aclz ✓ SIGNED
The altimeter's own compressed log, exactly as the device wrote it. This is the file to keep for a record claim.
11 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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