Vzdálenost
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Rychlost
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Zrychlení
Zvolte jednotku zrychlení: m/s² nebo G
Let 1796

Lil Nuke - Flight with 4 altimeters - 4

Nano V1 Rev 4 · firmware 1.52
Apogeum
756.77m
11.44 s after launch
Max. stoupání
159.42m/s
peak ascent
Max. při spalování
17.67G
during the burn
Přistání
129.16s
touchdown 7.05 m/s
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The flight, moment by moment

Liftoff
0 s
Náklon rampy23.91°
Thrust calc pad tilt2.3°
Launch detected
0.631 s
Výška30.04 m
Rychlost74.84 m/s
Vyhoření (první)
1.4 s
Výška127.88 m
Rychlost154.080 m/s
Možné vypuštění
11.054 s
Výška753.53 m
Rychlost10.48 m/s
Apogeum
11.44 s
Výška756.77 Metry
Max. náklon do vyhoření27.43°
Přistání
129.16 s
Výška-2.02 m
Max. klesání-12.65 m/s

Stabilita86.2%Výborný

Náklon při dohoření (20%)94
20% · Launch tilt 2.3°
Klápění/zatáčení (30%)93.8
25% · Coning 25.5/53.2°/s
Coning · boost (25%)77.9
25% · Spin 445.9°/s
Přímost tahu (15%)81.5
30% · Thrust 96.1%

Rocket information

Calculated from the flight data alone
Boost acceleration110.1 m/s²
average over the burn · 11.2 g
Coast deceleration15.3 m/s²
average · gravity plus drag
Ballistic coefficient534 kg/m²
fitted to the 10.04 s coast
Apogee lost to tilt0.6 m
flown vertical ≈ 757.3 m · from the thrust-calculated tilt
Chute opening peak38.07 G
largest deceleration after ejection
Average descent rate6.39 m/s
ejection to landing · 118.11 s
Baterie & teplota 92% → 90% · Teplota začátek 28.77 → 30.65 °C · Start po zapnutí 7m 5s

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
Apogeum756.77 Metry
Čas do apogea11.44 s
Výška vyhoření127.88 m
Výška max. rychlosti140.53 m
Výška vypuštění753.53 m
Výška přistání-2.02 m
Výška záznamu43.19 m
Rychlost
Max. stoupání159.41 m/s
Max. klesání-12.65 m/s
Při vyhoření154.080 m/s
Rychl. klesání-6.491 m/s
Rychl. vypuštění10.48 m/s
Rychl. přistání-7.046 m/s
Zrychlení
Max. při spalování17.67 G
Max. stoupání31.09 G
Max. klesání38.07 G
Prúm. stoupání1.22 G
Prúm. spalování12.13 G
Časy
Vyhoření (první)1.4 s
Apogeum11.44 s
Možné vypuštění11.054 s
Přistání129.16 s
Úhly
Náklon rampy23.91°
Thrust calc pad tilt2.3°
Max. náklon do vyhoření27.43°
Klápění při startu17.61°
Klopní při startu15.84°
Max. rotace (spal.)738.22 dps
Prúm. rotace (spal.)385.51 dps
Recovery
Single deploy
No dual deploy detected on this flight.
Obecné
Datum nahrání17/06/26-19:00:48
Datové vzorky11575
Celkový čas záznamu147.985 s
Prúm. vzorký/s78.2
Počet blokování0
Start po zapnutí7m 5s
Referenční osaX
Baterie & teplota
Baterie začátek92%
Baterie konec90%
Teplota začátek28.77°C
Teplota konec30.65°C
Uživatelské poznámky

A test of 2x Mercury and 2x Nano altimeters in a Lil Nuke with a G80 Aerotech motors.

Přidejte toto zařízení ke svému účtu pro úpravy
Youtube video
Žádné video
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Obrázky letu 0
Žádné obrázky
Skupiny
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
Active
1 photo
My Lil Nuke #1
LOC Precision — Lil' Nuke
8 flights linked
Type
Kit build
Diameter
57.4mm
Length
749.3mm
Dry weight
368.5g
Mod
Modified
Stages
1
Fins
3
Recovery
Parachute
Chute
61cm
Body
Loc paper tube
💬 7 comments · 👍 2 reactions
Sim data from sim files
MotorAltVelAccelApogeeSource
Estes A8-3135.3 m64.8 m/s29.6 G4.5 sRockSim (estes_viking.rkt)
Estes B4-4282.9 m105.3 m/s30.0 G6.1 sRockSim (estes_viking.rkt)
Estes B6-4288.1 m116.9 m/s31.0 G5.9 sRockSim (estes_viking.rkt)
Estes C6-5475.1 m171.4 m/s34.4 G7.5 sRockSim (estes_viking.rkt)
Estes C6-7483.1 m171.4 m/s34.4 G8.1 sRockSim (estes_viking.rkt)

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.

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.

Site nameUnnamed siteLat52.667949Lng-1.522803Ground level108.0 m · 354 ftDatum startu2026-06-14Čas startu14:00
Animace dat letu

FLIGHT 1796

756.77 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
Revision 4
Nano V1
Tento let byl proveden na Nano V1.
The hardware
Verze hardwareRev 4
Verze software1.52
Naposledy online17/06/26-19:00:48
Snímač tlakuBosch BMP 581
Akcelerometr32G 3-axis
Gyroskop2000 dgps 3-axis

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 (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.
AKTIVOVÁNO (22 samples / 130ms)
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
Kalibrace senzorú
Kalibrační offsety použité pro tento let.
Gyroskop
X2.000°
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
1796.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
887 KB
WX
1796_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 2026-06-14 14:00 local time at 52.6679, -1.5228.
196 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.

Let
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