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Prędkość
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Przyspieszenie
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Lot 3004

Nova Payloader (6) flight 38

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
105.35m
4.69 s after launch
Maks. wznoszenie
47.28m/s
peak ascent
Maks. podczas spalania
20.92G
during the burn
Lądowanie
25.81s
touchdown 4.96 m/s
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Podsumowanie lotu

The flight, moment by moment

Liftoff
0 s
Nachylenie rampy60.48°
Thrust calc pad tilt0.8°
Wypalenie (pierwszy)
0.32 s
Wysokość9.87 m
Prędkość47.090 m/s
Launch detected
0.781 s
Wysokość30.04 m
Prędkość40.04 m/s
Apogeum
4.69 s
Wysokość105.35 Metry
Maks. nachylenie do wypalenia9.45°
Možliwy wyrzut
5.267 s
Wysokość103.67 m
Prędkość-5.29 m/s
Lądowanie
25.8 s
Wysokość-0.6 m
Maks. opadanie-7.93 m/s

Stabilność81.1%Dobry

Nachylenie przy wypaleniu (20%)97.9
20% · Launch tilt 0.8°
Prędkość pochylania/odchylania (30%)92.3
25% · Coning 28.7/75.7°/s
Coning · boost (25%)63.5
25% · Spin 186.7°/s
Prostoliniowość ciągu (15%)75.2
30% · Thrust 94.7%

Rocket information

Calculated from the flight data alone
Boost acceleration147.2 m/s²
average over the burn · 15.0 g
Coast deceleration10.8 m/s²
average · gravity plus drag
Ballistic coefficient251 kg/m²
fitted to the 4.37 s coast
Apogee lost to tilt0.01 m
flown vertical ≈ 105.3 m · from the thrust-calculated tilt
Chute opening peak35.14 G
largest deceleration after ejection
Average descent rate5.07 m/s
ejection to landing · 20.53 s
Bateria & temperatura 74% → 70% · Temperatura początek 35.54 → 38.01 °C · Start po włączeniu 4m 33s

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.

Nachylenie przy wypaleniu (20%)20%How close to vertical it left the rod.
Prędkość pochylania/odchylania (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.
Prostoliniowość ciągu (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.

Wysokość
Apogeum105.35 Metry
Czas do apogeum4.69 s
Wysokość wypalenia9.87 m
Wys. maks. prędkości10.85 m
Wys. wyrzutu103.67 m
Wys. lądowania-0.6 m
Wysokość nagrywania-22.97 m
Prędkość
Maks. wznoszenie47.27 m/s
Maks. opadanie-7.93 m/s
Przy wypaleniu47.090 m/s
Prędk. opadania-4.924 m/s
Prędk. wyrzutu-5.29 m/s
Prędk. lądowania-4.961 m/s
Przyspieszenie
Maks. podczas spalania20.92 G
Maks. wznoszenie20.92 G
Maks. opadanie35.14 G
Śr. wznoszenie0.38 G
Śr. spalanie15.25 G
Czasy
Wypalenie (pierwszy)0.32 s
Apogeum4.69 s
Možliwy wyrzut5.267 s
Lądowanie25.8 s
Kąty
Nachylenie rampy60.48°
Thrust calc pad tilt0.8°
Maks. nachylenie do wypalenia9.45°
Przechylenie startowe-13.49°
Pochylenie startowe59.50°
Maks. obrót (spal.)307.35 dps
Śr. obrót (spal.)180.52 dps
Staging
Stages detected1
Burnout (refined)0.323 s
Stage S1 burnout
flip0.320 s
drag0.320 s
sig0.471 s
Recovery
Single deploy
No dual deploy detected on this flight.
Ogólne
Data przesłania28/09/26-22:44:06
Próbki danych8407
Całkowity czas nagrania42.777 s
Śr. próbki/s196.5
Liczba blokad0
Start po włączeniu4m 33s
Oś referencyjnaX
Bateria & temperatura
Bateria początek74%
Bateria koniec70%
Temperatura początek35.54°C
Temperatura koniec38.01°C
Notatki užytkownika

Adrel ALT-BMP also aboard. It reported 104.5m at 15ºC and filtered.

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Zdjęcia lotu 0
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Silniki lotu
1st stage · 5s delay
1×B14T-5QuestDetails
Burn time
0.38 s
Diameter
18.00 mm
Average thrust
13 N
Max thrust
17.65 N
Total weight
16.10 g
Propellant weight
2.30 g
Propellant type
Blue Thunder
Impulse4.97Ns
Max thrust17.6N
Burn time0.38s
Impulse classB
1st stage thrustloading curve…
Motor data by ThrustCurve.org
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Powiązana rakieta
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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 mass92.6gestimated
Mass at burnout90.3gestimated
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.

✓The altimeters aboard agree on apogee within 0.7%
Apogee spread104.6 – 179.5 m
#3007 · Nano V1Same rocket · same day179.5 mView flight →
#3005 · ThirdpartySame flight · another altimeter104.6 mView flight →

Miejsce startu, data i godzina

Kliknij na mapę, aby oznaczyć miejsce startu. Przełączaj między widokiem mapy i satelity.

Imagery © Esri, Maxar, Earthstar Geographics

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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.

Animacja danych lotu

FLIGHT 3004

105.35 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

Uwaga: Animacja lotu wymaga montażu wysokościomierza w stałej orientacji. Skalibruj czujniki dla najlepszych wyników.
Nano V1
Revision 4
Nano V1
Ten lot został wykonany na Nano V1.
The hardware
Wersja sprzętuRev 4
Wersja oprogramowania1.65
Ostatnio online28/09/26-22:44:06
Czujnik ciśnieniaBosch BMP 581
Akcelerometr32G 3-axis
Gyroskop2000 dgps 3-axis

Flights from this altimeter

6 of 6

Settings, as they were for this flight

Ogólne ustawienia lotu
Ciśnienie prognozowane
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
Detekcja startu
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.
WŁĄCZONY (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
Kalibracja czujników
Przesunięcia kalibracji użyte w tym locie.
Gyroskop⚠ Gyroskop nie został skalibrowany
X0.000°
Y0.000°
Z0.000°
Akcelerometr⚠ Akcelerometr nie został skalibrowany
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
3004.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
788 KB
LOG
3004.aclz ✓ SIGNED
The altimeter's own compressed log, exactly as the device wrote it. This is the file to keep for a record claim.
84 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.

Lot
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