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 3003

Nova Payloader (6) flight 37

Nano V1 Rev 4 · 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
78.61m
4.51 s after launch
Max. stijging
38.38m/s
peak ascent
Max. tijdens verbranding
7.32G
during the burn
Landing
21.25s
touchdown 3.5 m/s
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s
Toon gebeurtenissen
Temp. & druk aanpassen ?
Afbeelding
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Klik en sleep, of knijp op mobiel
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Vluchtsamenvatting

The flight, moment by moment

Liftoff
0 s
Helling lanceerplatform61.84°
Thrust calc pad tilt1.6°
Uitbranding (eerste)
0.95 s
Hoogte17.5 m
Snelheid38.280 m/s
Launch detected
1.3 s
Hoogte30.04 m
Snelheid33.61 m/s
Apogeum
4.5 s
Hoogte78.61 Meter
Max. helling tot uitbranding9.27°
Mogelijke uitwerping
5.845 s
Hoogte69.21 m
Snelheid-14.15 m/s
Landing
21.24 s
Hoogte-1.33 m
Max. daling-16.14 m/s

Stabiliteit90.2%Uitstekend

Helling bij burnout (20%)96
20% · Launch tilt 1.6°
Stamp/gier snelheid (30%)94
25% · Coning 25.2/34.6°/s
Coning · boost (25%)89.2
25% · Spin 143.7°/s
Stuwkrachtrechtheid (15%)83.9
30% · Thrust 96.6%

Rocket information

Calculated from the flight data alone
Boost acceleration40.3 m/s²
average over the burn · 4.1 g
Coast deceleration10.8 m/s²
average · gravity plus drag
Ballistic coefficient137 kg/m²
fitted to the 3.55 s coast
Apogee lost to tilt0.03 m
flown vertical ≈ 78.6 m · from the thrust-calculated tilt
Chute opening peak37.57 G
largest deceleration after ejection
Average descent rate4.58 m/s
ejection to landing · 15.39 s
Batterij & temperatuur 92% → 88% · Temperatuur start 33.15 → 35.42 °C · Lancering na inschakelen 3m 14s

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
Apogeum78.61 Meter
Tijd tot apogeum4.5 s
Hoogte uitbranding17.5 m
Hoogte max. snelheid16.54 m
Hoogte uitwerping69.21 m
Hoogte landing-1.33 m
Opnamehoogte-24.39 m
Snelheid
Max. stijging38.37 m/s
Max. daling-16.14 m/s
Bij uitbranding38.280 m/s
Snelheid daling-4.825 m/s
Snelheid uitwerping-14.15 m/s
Snelheid landing-3.504 m/s
Versnelling
Max. tijdens verbranding7.32 G
Max. stijging7.32 G
Max. daling37.57 G
Gem. stijging0.22 G
Gem. verbranding4.13 G
Tijden
Uitbranding (eerste)0.95 s
Apogeum4.5 s
Mogelijke uitwerping5.845 s
Landing21.24 s
Hoeken
Helling lanceerplatform61.84°
Thrust calc pad tilt1.6°
Max. helling tot uitbranding9.27°
Rol bij lancering-28.76°
Stamp bij lancering-57.38°
Max. rotatie (verbr.)233.2 dps
Gem. rotatie (verbr.)145.63 dps
Staging
Stages detected1
Burnout (refined)0.965 s
Stage S1 burnout
flip0.945 s
drag0.962 s
sig1.098 s
Recovery
Single deploy
No dual deploy detected on this flight.
Algemeen
Uploaddatum28/09/26-22:07:49
Datapunten8408
Totale opnametijd37.647 s
Gem. monsters/s223.3
Aantal vergrendelingen0
Lancering na inschakelen3m 14s
Referentie-asX
Batterij & temperatuur
Batterij start92%
Batterij einde88%
Temperatuur start33.15°C
Temperatuur einde35.42°C
Gebruikersnotities

Crackly and smoky boost from two-year-old B6W. Deploy well over the top, but good 'chute. Adrel ALT-BMP reported 78.4m apogee at 15ºC, filtered.

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Vluchtafbeeldingen 0
Geen afbeeldingen
Vluchtmotoren
1st stage · 4s delay
1×B6W-4QuestDetails
Burn time
1.17 s
Diameter
18.00 mm
Average thrust
4.22 N
Max thrust
9.13 N
Total weight
19.30 g
Propellant weight
2.80 g
Propellant type
White Lightning
Impulse4.87Ns
Max thrust9.1N
Burn time1.17s
Impulse classB
1st stage thrustloading curve…
Motor data by ThrustCurve.org
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Gekoppelde raket
Active
1 photo
Nova Payloader (6)
Estes Industries — Nova Payloader
3 flights linked
Type
Kit build
Diameter
25mm
Length
552mm
Dry weight
53g
Mod
Modified
Stages
1
Fins
3
Recovery
Parachute
Chute
30cm
Body
Kraft paper
💬 No comments yet
Flight mass
Liftoff mass99gestimated
Mass at burnout96.2gestimated
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.

Other flights on this motor

1 · highest first

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 agree on apogee within 0.6%
Apogee spread78.1 – 179.5 m
#3024 · ThirdpartySame flight · another altimeter78.1 mView flight →
#3007 · Nano V1Same rocket · same day179.5 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.

Site nameSixty Acres Park NorthLat47.705905Lng-122.138491Ground level10.0 m · 33 ftLanceerdatum2026-09-28Lanceertijd14:02
Vluchtdata-animatie

FLIGHT 3003

78.61 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
Softwareversie1.65
Laatst online28/09/26-22:07:49
DruksensorBosch BMP 581
Versnellingsmeter32G 3-axis
Gyroscoop2000 dgps 3-axis

Flights from this altimeter

6 of 6

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 (46 samples / 114.88ms)
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.
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
Sensorkalibratie
Kalibratie-offsets gebruikt voor deze vlucht.
Gyroscoop⚠ Gyroscoop is niet gekalibreerd
X0.000°
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
3003.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
787 KB
LOG
3003.aclz ✓ SIGNED
The altimeter's own compressed log, exactly as the device wrote it. This is the file to keep for a record claim.
78 KB
WX
3003_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 2026-09-28 14:02 local time at 47.7059, -122.1385.
1000 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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