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Prędkość
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Przyspieszenie
Wybierz jednostkę przyspieszenia: m/s² lub G

Nova Payloader (6) flight 43

Nano V1 Rev 4 · firmware 2.00Secure 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
330.35m
7.7 s after launch
Maks. wznoszenie
124.61m/s
peak ascent
Maks. podczas spalania
28.34G
during the burn
Lądowanie
86.06s
touchdown 4.45 m/s
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Podsumowanie lotu

The flight, moment by moment

Liftoff
0 s
Kąt rampy8.3°
Zejście z rampy2.41°
Launch detected
0.61618 s
Wysokość30.2 m
Prędkość115.75 m/s
Wypalenie (pierwszy)
0.7 s
Wysokość0 m
Prędkość124.600 m/s
Apogeum
7.69 s
Wysokość330.35 Metry
Maks. nachylenie do wypalenia11.69°
Možliwy wyrzut
7.945 s
Wysokość0 m
Prędkość m/s
Lądowanie
86.05 s
Wysokość0 m
Maks. opadanie-6.92 m/s

Stabilność92.4%Doskonały

Nachylenie przy wypaleniu (20%)79
20% · Rail angle 8.3°
Prędkość pochylania/odchylania (30%)98.4
25% · Coning 12.4/22.1°/s
Coning · boost (25%)95.3
25% · Spin 463.9°/s
Prostoliniowość ciągu (15%)94
30% · Thrust 98.8%

Rocket information

Calculated from the flight data alone
Boost acceleration178.0 m/s²
average over the burn · 18.2 g
Coast deceleration17.8 m/s²
average · gravity plus drag
Ballistic coefficient232 kg/m²
fitted to the 6.99 s coast
Apogee lost to tilt6.93 m
flown vertical ≈ 337.2 m · from the tilt at burnout
Chute opening peak38.36 G
largest deceleration after ejection
Bateria & temperatura 69% → 65% · Temperatura początek 29.78 → 32.72 °C · Start po włączeniu 30m 56s

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
Apogeum330.35 Metry
Czas do apogeum7.69 s
Wysokość wypalenia0 m
Wys. maks. prędkości40.98 m
Wys. wyrzutu0 m
Wys. lądowania0 m
Wysokość nagrywania1263.08 m
Prędkość
Maks. wznoszenie124.6 m/s
Maks. opadanie-6.92 m/s
Przy wypaleniu124.600 m/s
Prędk. opadania-4.214 m/s
Prędk. wyrzutu m/s
Prędk. lądowania-4.451 m/s
Przyspieszenie
Maks. podczas spalania28.34 G
Maks. wznoszenie28.34 G
Maks. opadanie38.36 G
Śr. wznoszenie1.55 G
Śr. spalanie18.48 G
Czasy
Wypalenie (pierwszy)0.7 s
Apogeum7.69 s
Možliwy wyrzut7.945 s
Lądowanie86.05 s
Kąty
Kąt rampy ?8.3° ± 0.32°
Zejście z rampy ?2.4°
Maks. nachylenie do wypalenia ?11.69°
Orientacja ?21.12°
Przesunięcie montażu ?13.1°
Przechylenie startowe2.05°
Pochylenie startowe21.03°
Maks. obrót (spal.)801.14 dps
Śr. obrót (spal.)394.74 dps
Staging
Stages detected1
Burnout (refined)0.729 s
Stage S1 burnout
flip0.704 s
drag0.729 s
sig0.854 s
Recovery
Single deploy
No dual deploy detected on this flight.
Ogólne
Data przesłania27/10/26-03:37:09
Próbki danych12757
Całkowity czas nagrania98.805 s
Śr. próbki/s129.1
Liczba blokad0
Start po włączeniu30m 56s
Oś referencyjnaX
Bateria & temperatura
Bateria początek69%
Bateria koniec65%
Temperatura początek29.78°C
Temperatura koniec32.72°C
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Tell us what looks wrong and we'll look into it. It helps us find and fix problems in the firmware and on the site, and we can correct this flight.
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Notatki užytkownika

Silicdyne Reperix reported 351 meters apogee. Speeds and accelerations were nonsense.

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Zdjęcia lotu 1
Flown as
Rocket
Estes Industries
Motor configuration
Custom
1× Quest D16-6, set on this flight
Loaded weight
75.0 g
set on this flight · estimated 91.4 g from the rated impulse

Measured burn

from this flight’s thrust and its loaded weight
Total impulse, NFPA 112510.00 Ns
rated 12.40 Ns, 19.4% under, within the 20% NFPA 1125 allows
Total impulse, absolute10.00 Ns
Measured asC14
sold as a D16
Burn time, NFPA 11250.72 s
0.00 to 0.72 s
Average thrust14.0 N
impulse over burn time
Peak thrust20.6 N
at 0.59 s
Specific impulse82 s
12.5 g of propellant
Mass at burnout62.5 g
loaded weight less propellant
NFPA 1125, the code motors are certified to by NAR, Tripoli and CAR: the burn runs from where the thrust first rises above 5% of its peak to where it falls below it (7.8.3), and the total impulse from that rise to the last measurable thrust before ejection (7.8.5). Absolute counts every newton from liftoff. The same code lets a production lot vary 20% from its mean impulse for a model rocket motor and 10% for high power (7.8.6). Both figures follow the loaded weight: 1% out on the weight is about 1% out on the impulse.
Silniki lotu
1st stage · 6s delay
1×D16-6QuestDetails
Burn time
0.79 s
Diameter
18.00 mm
Average thrust
15.6 N
Max thrust
22.3 N
Total weight
25.60 g
Propellant weight
12.50 g
Propellant type
Black Max
Impulse12.4Ns
Max thrust22.3N
Burn time0.79s
Impulse classD
1st stage thrustloading curve…
Motor data by ThrustCurve.org
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Powiązana rakieta
Active
1 photo
Nova Payloader (6)
Estes Industries — Nova Payloader
8 flights linked
Type
Kit build
Diameter
25mm
Length
552mm
Empty weight
53g
Mod
Modified
Stages
1
Fins
3
Recovery
Parachute
Chute
30cm
Body
Kraft paper
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Other flights on this motor

1 · highest first

Linked flights

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Miejsce startu, data i godzina

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

Imagery © Esri, Maxar, Earthstar Geographics

Kliknij na mapę · Przeciągnij, aby dostosować

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 namePlayas Training Center - NSL WestLat31.943667Lng-108.548579Ground level1350.8 m · 4432 ftData startu2026-10-26Godzina startu09:45
Animacja danych lotu

FLIGHT 3168

330.35 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
Rocketry Ltd

Nano V1

Kompaktowy altimetr do małych rakiet. Ten lot został wykonany na Nano V1.
Wersja sprzętu Rev 4Wersja oprogramowania 2.00Ostatnio online 27/10/26-03:37:09

Specyfikacja

Elektronika

Mikrokontroler
ESP32-S232-bit ESP32-S2 240MHz
Akcelerometr
ST LSM6DSO3232G 3-axis (SPI)
Barometr
Bosch BMP581300 to 1250 hPa within specification
Żyroskop
ST LSM6DSO322000 dgps 3-axis

Rejestracja danych

Maksymalna częstotliwość próbkowania
833 Hz
Maks. liczba próbek w zapisie
38,000
Najdłuższy zapis
1 h 3 minAt 10Hz although default settings are 433Hz with 1:8 hybrid mode

Elektronika

Mikrokontroler
ESP32-S232-bit ESP32-S2 240MHz
Akcelerometr
ST LSM6DSO3232G 3-axis (I2C)
Barometr
Bosch BMP581300 to 1250 hPa within specification
Żyroskop
ST LSM6DSO322000 dgps 3-axis

Rejestracja danych

Maksymalna częstotliwość próbkowania
833 Hz
Maks. liczba próbek w zapisie
38,000
Najdłuższy zapis
1 h 3 minAt 10Hz although default settings are 433Hz with 1:8 hybrid mode

Wymiary, waga i bateria

Wymiary
20 × 10 × 8.9 mm
Waga
1.65 g1.65 g z najmniejszą baterią
Napięcie baterii
3 do 4.2 V
Czas pracy na baterii
5na najmniejszej baterii
Wymiary
20 × 10 × 8.9 mm
Waga
1.65 g1.65 g z najmniejszą baterią
Napięcie baterii
3 do 4.2 V
Czas pracy na baterii
5na najmniejszej baterii

Dokumenty

Flights from this altimeter

20 of 3120 of 117

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 (417Hz)
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.
417 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 (44 samples / 109.42ms)
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.
Attitude filter 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
3168.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
1248 KB
LOG
3168.aclz ✓ SIGNED
The altimeter's own compressed log, exactly as the device wrote it. This is the file to keep for a record claim.
123 KB
WX
3168_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 2026-10-26 09:45 local time at 31.9437, -108.5486.
1412 KB
Pobierz
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.

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