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Vol 2905

Flight 2905

Mercury V1 Rev 1 · firmware 1.24B
Apogée
22.14m
2.3 s after launch
Max. montée
27.96m/s
peak ascent
Max. pendant combustion
16.61G
during the burn
Atterrissage
4.47s
touchdown 5.08 m/s
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Résumé du vol

The flight, moment by moment

Liftoff
0 s
Inclinaison rampe5.75°
Thrust calc pad tilt5.5°
Launch detected
0.126 s
Altitude3.97 m
Vitesse24.36 m/s
Fin combustion (premier)
0.3 s
Altitude11.02 m
Vitesse27.540 m/s
Apogée
2.3 s
Altitude22.14 Mètres
Incl. max. jusqu’à fin comb.5.96°
Atterrissage
4.46 s
Altitude2.85 m
Max. descente-11.3 m/s

Stabilité96.2%Excellent

Inclinaison à la fin de combustion (20%)86.2
20% · Launch tilt 5.5°
Tangage/lacet (30%)99.3
25% · Coning 7.9/0.3°/s
Coning · boost (25%)99.9
25% · Spin 149.2°/s
Rectitude de poussée (15%)97.1
30% · Thrust 99.5%

Rocket information

Calculated from the flight data alone
Boost acceleration91.8 m/s²
average over the burn · 9.4 g
Coast deceleration13.8 m/s²
average · gravity plus drag
Ballistic coefficient6 kg/m²
fitted to the 2.00 s coast
Apogee lost to tilt0.1 m
flown vertical ≈ 22.2 m · from the thrust-calculated tilt
Chute opening peak1.27 G
largest deceleration after ejection
Batterie & température 0% → 0% · Température début 27.56 → 26.78 °C · Lancement après démarrage 1m 39s

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
Apogée22.14 Mètres
Temps jusqu’apogée2.3 s
Altitude fin combustion11.02 m
Altitude vitesse max.12.13 m
Altitude éjection0.17 m
Altitude atterrissage2.85 m
Altitude enregistrement40.49 m
Vitesse
Max. montée27.96 m/s
Max. descente-11.3 m/s
À fin combustion27.540 m/s
Vitesse descente-5.963 m/s
Vitesse éjection13.48 m/s
Vitesse atterrissage-5.075 m/s
Accélération
Max. pendant combustion16.61 G
Max. montée16.61 G
Max. descente1.27 G
Moy. montée-0.11 G
Moy. combustion4.42 G
Temps
Fin combustion (premier)0.3 s
Apogée2.3 s
Éjection possible0 s
Atterrissage4.46 s
Sortie #1 ON0 s
Sortie #1 OFF0 s
Angles
Inclinaison rampe5.75°
Thrust calc pad tilt5.5°
Incl. max. jusqu’à fin comb.5.96°
Roulis au lancement-3.83°
Tangage au lancement-4.28°
Rotation max. (comb.)180 dps
Rotation moy. (comb.)88.51 dps
Recovery
Single deploy
No dual deploy detected on this flight.
Général
Date envoi12-Sep at 13:27
Échantillons638
Durée totale enregistrement20.200 s
Moy. échantillons/s31.5
Nombre de verrouillages1
Lancement après démarrage1m 39s
Axe de référenceX
Batterie & température
Batterie début0%
Batterie fin0%
Température début27.56°C
Température fin26.78°C
Temp. MT1 lancement0°C
Règles de sortie
Aucune règle configurée
Notes utilisateur
Aucune note
Ajoutez cet appareil à votre compte pour modifier
Vidéo Youtube
Aucune vidéo
Ajoutez cet appareil à votre compte pour modifier
Images du vol 0
Aucune image
Moteurs du vol
Aucun moteur ajouté à ce vol
Ajoutez cet appareil à votre compte pour modifier
Fusée associée
Aucune fusée associée à ce vol
Règles de sortie
Règles de sortie were not available until firmware 2.0
Correspondance moteur (BETA)
Encore en phase de test ! Nous cherchons à deviner quel moteur a été utilisé.
Marque
Moteur
Score
Forme
Comb.
Estes
1/2A3T
123
95.7%
90.3%
Cesaroni
68-F240-VM-15A
115
96.5%
80.5%
AeroTech
H669N
90
93.1%
83.6%
Quest
B14T
88
98.4%
91.4%
Estes
1/2A6
77
90%
85.1%
AeroTech
I1299N
67
91.8%
88.4%
Cesaroni
H410-VM
48
94.2%
86.4%
Estes
1/4A3T
40
92.6%
89.7%
AeroTech
H999
33
94.4%
81.8%
Cesaroni
F120-VM
11
88.8%
85.4%

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.

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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

No launch site has been set for this flight.

Animation des données

FLIGHT 2905

22.14 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.
Mercury V1
Revision 1
Mercury V1
Ce vol a été effectué sur un Mercury V1.
The hardware
Version matérielRev 1
Version logiciel1.24B
Dernière connexion12-Sep at 17:24
Capteur pressionBosch BMP 390
Accéléromètre32G 3-axis
Gyroscope2000 dgps 3-axis
MagnétomètreN/A

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.
1019 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.
2 meters
Fréquence échantillonnage
i
The base sample rate of the altimeter's sensors in samples per second. This setting was deprecated in firmware 2.0+.
32 Hz
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:
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.
0
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: 450 samples stable (~9s)
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.
4x 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 3
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.
Kalman 2 (default)
Temps verrouillage
i
The Lockout time is how long the altimeter should stop making decisions and taking actions if it detects unusual high speed altitude changes that are unexpected.
These false readings can be caused by ejection charges (if the altimeter is in the same compartment as the motor ejection gases) or even when you transition to Mach speeds and can give false readings of altitude changes.

When these events are detected the system enters Lockout for the specified time while it stabalises. This effects things like triggering the output, or calculating other data.
750ms
Changement verrouillage
i
This is how we detect a lockout. If the pressure changes by this much in a single sample downwards (pressure increase, lower altitude) then it's likely to be a false reading. Multiply the setting by 32 to get the speed in meters per second that it will trigger at.
1.5 meters
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 (6 samples / 196.00ms)
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.
Upwards (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.
1.4G
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
Capteur temp.
i
If an external MT1 temperature sensor is connected, this controls whether it is used for logging only or also for altitude calculations.
Paramètres de sortie
Sortie 1 activée
i
Disable or enable the output from being able to turn on or off.
DÉSACTIVÉ
Sortie 1 déclencheur
i
After apogee (altitude)
This method triggers when the altitude drops below the set altitude after apogee is detected.
After apogee (time)
This method triggers the defined seconds after apogee is detected.
After launch (altitude)
This method is activated if/once the altimeter exceeds the set altitude after launch.
After launch (time)
This option triggers the defined seconds after launch is detected.
After burnout (time)
This method triggers the defined seconds after burnout is detected.
After apogee (altitude)
Sortie 1 durée
i
This is how long the output should trigger ON state when the rules are met.
2000ms
Sortie 1 altitude
i
This is the altitude to trigger at if using a trigger method that works on altitude.

For example if you set this to 75m and After apogee (altitude) for the trigger then the output will turn on at 75m on descent above the launch altitude.
0 meters
Sortie 1 temps
i
This is the time variable for output triggers that work on time.

For example if you set this to 3 seconds and After apogee (time) as the trigger then the output will turn on 3 seconds after apogee.
0 seconds
Verrouillage altitude
i
Altitude lock is a safety feature that prevents the output from triggering if the altitude is below this level when the rules are met.
50.00 m
Verrouillage inclinaison
i
This is another safety feature. It can be used to disable the output if the rocket has gone too far from vertical.

For example if you set the tilt angle lock to 40 degrees then the output will not fire if the rocket is more than 40 degrees from vertical. To disable set this to 0.
0.00 °
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
Paramètres appareil
TAG appareil
i
A custom name or tag assigned to this device for easy identification.
ScoutsDBDC
Langue
i
The language setting configured on the device.
en
Mode arrêt
i
Controls what happens after recording. Standard shuts down normally, Delayed keeps WiFi on for 30 seconds after landing, Stay on keeps the device powered on.
Delayed 30s
Luminosité LED
i
The brightness level of the LED indicators on the Mercury. Lower values save battery.
Puissance WiFi TX
i
WiFi transmit power level. Higher gives better range but uses more battery.
Mode veille
i
Controls whether the device enters low-power sleep when idle.
Stay awake
Surveillance batterie
i
Monitors battery voltage during the flight.
ENABLED
Groupe cloud
i
The cloud group / category this flight is assigned to.
Ports GP6 / GP7
Le contrôle des ports GP n’était pas disponible avant le firmware 2.0
Carte servo I2C PCA9685
Le contrôle des ports GP n’était pas disponible avant le firmware 2.0
Prédiction et aérofreins
Cette fonctionnalité n’était pas disponible avant la version 2.10+

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
2905.csv
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
49 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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