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Vol 2916

Lil Nuke - G80-10 - altimeter 4/4

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.
Apogée
823.05m
12.23 s after launch
Max. montée
163.6m/s
peak ascent
Max. pendant combustion
16.89G
during the burn
Atterrissage
132.86s
touchdown 7.95 m/s
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Résumé du vol

The flight, moment by moment

Liftoff
0 s
Inclinaison rampe22.41°
Thrust calc pad tilt1.8°
Launch detected
0.614 s
Altitude30.16 m
Vitesse91.56 m/s
Fin combustion (premier)
1.42 s
Altitude144.08 m
Vitesse162.790 m/s
Éjection possible
11.61 s
Altitude819.5 m
Vitesse4.28 m/s
Apogée
12.22 s
Altitude823.05 Mètres
Incl. max. jusqu’à fin comb.27.68°
Atterrissage
132.85 s
Altitude-5.32 m
Max. descente-11.83 m/s

Stabilité39%Correct

Inclinaison à la fin de combustion (20%)95.3
20% · Launch tilt 1.8°
Tangage/lacet (30%)56.7
25% · Coning 87.2/181.5°/s
Coning · boost (25%)23.2
25% · Spin 363°/s
Rectitude de poussée (15%)0
30% · Thrust 73.4%

Rocket information

Calculated from the flight data alone
Boost acceleration114.6 m/s²
average over the burn · 11.7 g
Coast deceleration15.1 m/s²
average · gravity plus drag
Ballistic coefficient557 kg/m²
fitted to the 10.80 s coast
Apogee lost to tilt0.4 m
flown vertical ≈ 823.4 m · from the thrust-calculated tilt
Chute opening peak39.31 G
largest deceleration after ejection
Average descent rate6.8 m/s
ejection to landing · 121.24 s
Batterie & température 90% → 82% · Température début 35.38 → 43.31 °C · Lancement après démarrage 14m 52s

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.

Inclinaison à la fin de combustion (20%)20%How close to vertical it left the rod.
Tangage/lacet (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.
Rectitude de poussée (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.

Altitude
Apogée823.05 Mètres
Temps jusqu’apogée12.22 s
Altitude fin combustion144.08 m
Altitude vitesse max.134.6 m
Altitude éjection819.5 m
Altitude atterrissage-5.32 m
Altitude enregistrement34.36 m
Vitesse
Max. montée163.59 m/s
Max. descente-11.83 m/s
À fin combustion162.790 m/s
Vitesse descente-6.744 m/s
Vitesse éjection4.28 m/s
Vitesse atterrissage-7.950 m/s
Accélération
Max. pendant combustion16.89 G
Max. montée24.88 G
Max. descente39.31 G
Moy. montée1.09 G
Moy. combustion11.95 G
Temps
Fin combustion (premier)1.42 s
Apogée12.22 s
Éjection possible11.61 s
Atterrissage132.85 s
Angles
Inclinaison rampe22.41°
Thrust calc pad tilt1.8°
Incl. max. jusqu’à fin comb.27.68°
Roulis au lancement22.36°
Tangage au lancement-1.42°
Rotation max. (comb.)1272.55 dps
Rotation moy. (comb.)353.96 dps
Staging
Stages detected1
Burnout (refined)1.457 s
Stage S1 burnout
flip1.415 s
drag1.471 s
sig1.567 s
Recovery
Single deploy
No dual deploy detected on this flight.
Général
Date envoi13/09/26-19:11:00
Échantillons16232
Durée totale enregistrement151.396 s
Moy. échantillons/s107.2
Nombre de verrouillages0
Lancement après démarrage14m 52s
Axe de référenceX
Batterie & température
Batterie début90%
Batterie fin82%
Température début35.38°C
Température fin43.31°C
Notes utilisateur

We flew 4x Nano altimeters together in this rocket on a G80-10 motor and a Loc Lil Nuke.
Tall the altimeters agreed within just 21cm

823.05m
822.84m
822.94m
823.05m

This represents an impressive success in our TrueFuse 2F fusion filter and the hardware and pressure sensor as a whole that all 4 altimeters agree so closely.

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Moteurs du vol
1st stage · 10s delay
G80T-10AeroTechDetails
Durée combustion
1.7 s
Diameter
29.00 mm
Poussée moyenne
77.6 N
Poussée max.
108.5 N
Poids total
127.90 g
Poids propergol
62.50 g
Type propergol
Blue Thunder
Impulsion136.6Ns
Poussée max.108.5N
Durée combustion1.7s
Classe impulsionG
1st stage thrustloading curve…
Motor data by ThrustCurve.org
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Fusée associée
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.

The altimeters aboard agree on apogee within 0%
Apogee spread822.8 – 823.1 m
#2915 · Nano V1Same flight · another altimeter823.1 mView flight →
#2914 · Nano V1Same flight · another altimeter822.9 mView flight →
#2913 · Nano V1Same flight · another altimeter822.8 mView flight →

Site de lancement, date & heure

Cliquez sur la carte pour marquer votre site de lancement. Basculez entre vue carte et satellite.

Imagery © Esri, Maxar, Earthstar Geographics

Cliquez sur la carte · Glissez pour ajuster

Site nameTwycrossLat52.668987Lng-1.523946Ground level106.2 m · 348 ftDate de lancement2026-09-13Heure de lancement13:45
Animation des données

FLIGHT 2916

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

Note : L’animation de vol nécessite que votre altimètre soit monté dans une orientation fixe. Calibrez vos capteurs pour de meilleurs résultats.
Nano V1
Revision 4
Nano V1
Ce vol a été effectué sur un Nano V1.
The hardware
Version matérielRev 4
Version logiciel1.65
Dernière connexion13/09/26-19:11:00
Capteur pressionBosch BMP 581
Accéléromètre32G 3-axis
Gyroscope2000 dgps 3-axis

Flights from this altimeter

No other flights yet. This will fill up as you fly.

Settings, as they were for this flight

Paramètres généraux
Pression prévue
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
Détection lancement
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
Ratio échantillonnage
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. échantillons
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
Arrêt enregistrement
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
Suréchantillonnage
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
Filtre IIR
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
Filtre pression
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
Synchro capteurs
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.
ACTIVÉ (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)
Filtre IMU
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
ALP lancement
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
Verrouillage lancement
i
When enabled, the altimeter locks out recording for a set period after power on to prevent false triggering during setup.
DISABLED
Température statique
i
A fixed temperature value used for altitude calculation when the external temperature sensor is disabled or not connected.
15 °C
Étalonnage capteurs
Décalages de calibration utilisés pour ce vol.
Gyroscope⚠ Le gyroscope n’a pas été calibré
X0.000°
Y0.000°
Z0.000°
Accéléromètre⚠ L’accéléromètre n’a pas été calibré
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
2916.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
1547 KB
LOG
2916.aclz ✓ SIGNED
The altimeter's own compressed log, exactly as the device wrote it. This is the file to keep for a record claim.
177 KB
WX
2916_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 2026-09-13 13:45 local time at 52.6679, -1.5228.
1077 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.

Vol
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