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 1719

200Hz Nano test (1)

Nano V1 Rev 4 · firmware 1.52
Apogeum
148.13m
4.45 s after launch
Max. stijging
52.72m/s
peak ascent
Max. tijdens verbranding
8.63G
during the burn
Landing
11.94s
touchdown 6.06 m/s
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Vluchtsamenvatting

The flight, moment by moment

Liftoff
0 s
Helling lanceerplatform19.89°
Thrust calc pad tilt6.9°
Launch detected
0.015 s
Hoogte30.47 m
Snelheid41.51 m/s
Uitbranding (eerste)
0.49 s
Hoogte53.97 m
Snelheid51.280 m/s
Apogeum
4.44 s
Hoogte148.13 Meter
Max. helling tot uitbranding48.59°
Mogelijke uitwerping
4.717 s
Hoogte147.97 m
Snelheid-0.62 m/s
Landing
11.94 s
Hoogte112.3 m
Max. daling-21.55 m/s

Stabiliteit20.2%Slecht

⚠ Low confidence — altimeter may have moved in flight
Helling bij burnout (20%)82.5
20% · Launch tilt 6.9°
Stamp/gier snelheid (30%)11.2
25% · Coning 281.4/502.6°/s
Coning · boost (25%)3.8
25% · Spin 204.5°/s
Stuwkrachtrechtheid (15%)0
30% · Thrust 77.8%

Rocket information

Calculated from the flight data alone
Boost acceleration104.7 m/s²
average over the burn · 10.7 g
Coast deceleration13.0 m/s²
average · gravity plus drag
Ballistic coefficient129 kg/m²
fitted to the 3.95 s coast
Apogee lost to tilt1.07 m
flown vertical ≈ 149.2 m · from the thrust-calculated tilt
Chute opening peak42.8 G
largest deceleration after ejection
Average descent rate4.93 m/s
ejection to landing · 7.22 s
Batterij & temperatuur 99% → 96% · Temperatuur start 20.64 → 15.14 °C · Lancering na inschakelen 1m 4s

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
Apogeum148.13 Meter
Tijd tot apogeum4.44 s
Hoogte uitbranding53.97 m
Hoogte max. snelheid50.18 m
Hoogte uitwerping147.97 m
Hoogte landing112.3 m
Opnamehoogte81.03 m
Snelheid
Max. stijging52.72 m/s
Max. daling-21.55 m/s
Bij uitbranding51.280 m/s
Snelheid daling-4.769 m/s
Snelheid uitwerping-0.62 m/s
Snelheid landing-6.063 m/s
Versnelling
Max. tijdens verbranding8.63 G
Max. stijging8.63 G
Max. daling42.8 G
Gem. stijging-0.42 G
Gem. verbranding1.45 G
Tijden
Uitbranding (eerste)0.49 s
Apogeum4.44 s
Mogelijke uitwerping4.717 s
Landing11.94 s
Hoeken
Helling lanceerplatform19.89°
Thrust calc pad tilt6.9°
Max. helling tot uitbranding48.59°
Rol bij lancering-15.12°
Stamp bij lancering-9.73°
Max. rotatie (verbr.)1260.33 dps
Gem. rotatie (verbr.)678.92 dps
Recovery
Single deploy
No dual deploy detected on this flight.
Algemeen
Uploaddatum08/06/26-21:20:10
Datapunten5871
Totale opnametijd42.228 s
Gem. monsters/s139
Aantal vergrendelingen0
Lancering na inschakelen1m 4s
Referentie-asX
Batterij & temperatuur
Batterij start99%
Batterij einde96%
Temperatuur start20.64°C
Temperatuur einde15.14°C
Gebruikersnotities
First test of the Nano altimeter at 200Hz for the new firmware. A small bug on the launch point look back but otherwise has worked rather well. The pre buffer scaling hasn't taken effect so there wasn't enough to have an accurate launch point or lookback, resolved with time based prebuffer rather than fixed sample number.

This flight was flown in the main tube exposed the ejection charge and out in the open air on descent. The True path filter has done a great job at cleaning up the noise and ejection charge pressure spike it would have seen.
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Vluchtafbeeldingen 0
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Vluchtmotoren
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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Gekoppelde raket
Active
1 photo
Klima Pegasus - Test Beast
Klima — Pegasus RTF
3 flights linked
Type
Kit build
Diameter
35mm
Length
495mm
Dry weight
80g
Stages
1
Recovery
Parachute
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Flight mass
Liftoff mass603gestimated
Mass at burnout593.4gestimated
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.

No linked flights yet.

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 1719

148.13 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
Softwareversie1.52
Laatst online08/06/26-21:20:10
DruksensorBosch BMP 581
Versnellingsmeter32G 3-axis
Gyroscoop2000 dgps 3-axis

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 (200Hz)
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.
200 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
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
1719.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
458 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.

Vlucht
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