Vzdálenost
Zvolte jednotku vzdálenosti: Metry(m), Stopy(ft), Míle(mi) nebo Kilometry(km)
Rychlost
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Zrychlení
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Lil Nuke - G80-10 - altimeter 3/4

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
823.05m
12.23 s after launch
Max. stoupání
168.06m/s
peak ascent
Max. při spalování
18.69G
during the burn
Přistání
132.98s
touchdown 7.95 m/s
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The flight, moment by moment

Liftoff
0 s
Úhel rampy5.3°
Odklon od rampy10.58°
Launch detected
0.615 s
Výška30.17 m
Rychlost94.83 m/s
Vyhoření (první)
1.4 s
Výška144.22 m
Rychlost166.970 m/s
Možné vypuštění
11.611 s
Výška819.45 m
Rychlost4.35 m/s
Apogeum
12.23 s
Výška823.05 Metry
Max. náklon do vyhoření10.89°
Přistání
132.98 s
Výška-5.95 m
Max. klesání-11.74 m/s

Stabilita85.7%Výborný

Náklon při dohoření (20%)86.7
20% · Rail angle 5.3°
Klápění/zatáčení (30%)95.3
25% · Coning 21.9/46.5°/s
Coning · boost (25%)82.1
25% · Spin 364.3°/s
Přímost tahu (15%)79.9
30% · Thrust 95.7%

Rocket information

Calculated from the flight data alone
Boost acceleration119.3 m/s²
average over the burn · 12.2 g
Coast deceleration15.4 m/s²
average · gravity plus drag
Ballistic coefficient531 kg/m²
fitted to the 10.83 s coast
Apogee lost to tilt0.15 m
flown vertical ≈ 823.2 m · from the tilt at burnout
Chute opening peak38.66 G
largest deceleration after ejection
Average descent rate6.8 m/s
ejection to landing · 121.37 s
Baterie & teplota 91% → 81% · Teplota začátek 35.09 → 41.85 °C · Start po zapnutí 14m 45s

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.

Náklon při dohoření (20%)20%How close to vertical it left the rod.
Klápění/zatáčení (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.
Přímost tahu (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.

Výška
Apogeum823.05 Metry
Čas do apogea12.23 s
Výška vyhoření144.22 m
Výška max. rychlosti140.37 m
Výška vypuštění819.45 m
Výška přistání-5.95 m
Výška záznamu34.21 m
Rychlost
Max. stoupání168.06 m/s
Max. klesání-11.74 m/s
Při vyhoření166.970 m/s
Rychl. klesání-6.722 m/s
Rychl. vypuštění4.35 m/s
Rychl. přistání-7.948 m/s
Zrychlení
Max. při spalování18.69 G
Max. stoupání24.85 G
Max. klesání38.66 G
Prúm. stoupání1.1 G
Prúm. spalování12.28 G
Časy
Vyhoření (první)1.4 s
Apogeum12.23 s
Možné vypuštění11.611 s
Přistání132.98 s
Úhly
Úhel rampy ?5.3° ± 0.25° nespolehlivé, držák se pohnul
Odklon od rampy ?10.6° nespolehlivé, držák se pohnul
Max. náklon do vyhoření ?10.89°
Orientace ?4.28°
Odchylka montáže ?3.4°
Klápění při startu0.01°
Klopní při startu-4.27°
Max. rotace (spal.)731.53 dps
Prúm. rotace (spal.)335.92 dps
Staging
Stages detected1
Burnout (refined)1.449 s
Stage S1 burnout
flip1.405 s
drag1.454 s
sig1.558 s
Recovery
Single deploy
No dual deploy detected on this flight.
Obecné
Datum nahrání13/09/26-19:10:32
Datové vzorky16292
Celkový čas záznamu151.403 s
Prúm. vzorký/s107.6
Počet blokování0
Start po zapnutí14m 45s
Referenční osaX
Baterie & teplota
Baterie začátek91%
Baterie konec81%
Teplota začátek35.09°C
Teplota konec41.85°C
Something look wrong with this flight's data?
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.
You're not logged in, so we can't let you know when we've looked into it.
Uživatelské poznámky
Žádné poznámky
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Youtube video
Žádné video
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Obrázky letu 0
Žádné obrázky
Flown as
Rocket
None
not linked
Motor configuration
Custom
1× AeroTech G80T-10, set on this flight
Loaded weight
706.5 g
estimated, none entered

Measured burn

from this flight’s thrust
Total impulse, NFPA 1125needs the weight
rated 136.6 Ns
Burn time, NFPA 11251.44 s
0.00 to 1.44 s
Peak thrustneeds the weight
at 0.01 s
With no loaded weight the impulse would only give the motor’s rating back, so it waits for the weight. The burn time is measured either way.
Motory letu
1st stage · 10s delay
1×G80T-10AeroTechDetails
Burn time
1.7 s
Diameter
29.00 mm
Average thrust
77.6 N
Max thrust
108.5 N
Total weight
127.90 g
Propellant weight
62.50 g
Propellant type
Blue Thunder
Impulse136.6Ns
Max thrust108.5N
Burn time1.7s
Impulse classG
1st stage thrustloading curve…
Motor data by ThrustCurve.org
Přidejte toto zařízení ke svému účtu pro úpravy
Propojená raketa
K tomuto letu není připojena žádná raketa

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%
Apogee spread823.05 – 823.1 m
#2916 · Nano V1Same flight · another altimeter823.1 mView flight →

Místo startu, datum a čas

Klikněte na mapu pro označení místa startu. Přepínejte mezi mapou a satelitním pohledem.

Imagery © Esri, Maxar, Earthstar Geographics

Klikněte na mapu · Přetáhněte pro úpravu

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.

Animace dat letu

FLIGHT 2915

823.05 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

Poznámka: Animace letu vyžaduje montáž výškoměru v pevné orientaci. Kalibrujte senzory pro nejlepší výsledky.
Nano V1
Rocketry Ltd

Nano V1

Kompaktní výškoměr pro malé rakety. Tento let byl proveden na Nano V1.
Verze hardware Rev 4Verze software 1.65Naposledy online 13/09/26-19:10:32

Specifikace

Elektronika

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

Záznam dat

Maximální vzorkovací frekvence
833 Hz
Max. počet vzorků v záznamu
38,000
Nejdelší záznam
1 h 3 minAt 10Hz although default settings are 433Hz with 1:8 hybrid mode

Elektronika

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

Záznam dat

Maximální vzorkovací frekvence
833 Hz
Max. počet vzorků v záznamu
38,000
Nejdelší záznam
1 h 3 minAt 10Hz although default settings are 433Hz with 1:8 hybrid mode

Rozměry, hmotnost a baterie

Rozměry
20 × 10 × 8.9 mm
Hmotnost
1.65 g1.65 g s nejmenší baterií
Napětí baterie
3 až 4.2 V
Výdrž baterie
5na nejmenší baterii
Rozměry
20 × 10 × 8.9 mm
Hmotnost
1.65 g1.65 g s nejmenší baterií
Napětí baterie
3 až 4.2 V
Výdrž baterie
5na nejmenší baterii

Dokumenty

Flights from this altimeter model

20 of 117

Settings, as they were for this flight

Obecná nastavení letu
Předpovězený tlak
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
Detekce 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.
AKTIVOVÁNO (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
Kalibrace senzorú
Kalibrační offsety použité pro tento let.
Gyroskop⚠ Gyroskop nebyl zkalibrován
X0.000°
Y0.000°
Z0.000°
Akcelerometr⚠ Akcelerometr nebyl zkalibrován
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
2915.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
1538 KB
LOG
2915.aclz ✓ SIGNED
The altimeter's own compressed log, exactly as the device wrote it. This is the file to keep for a record claim.
166 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.

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