Bem-vindo de volta
Inicie sessão na sua conta Altimeter Cloud
Não tem conta? Criar uma
Criar uma conta gratuita
Enviaremos um link de confirmação por e-mail. Verifique a pasta de spam se não o receber.
Já tem uma conta? Entrar
Início
Dispositivo: 1000-3BF4-4AFC
Voo ID: 1786Lil Nuke - Flight with 4 altimeters - 3
Mostrar eventos
Transferir
Ajustar temp. & pressão ?
Imagem
Conjuntos de dados
Clique na legenda para mostrar ou ocultar os dados
Zoom
Clique e arraste, ou belisque no telemóvel
Comparar voo ?
Resumo do voo
Altitude
Apogeu
756.68 Metros
Tempo até apogeu
11.42 seconds
Altitude fim combustão
129.76 m
Altitude vel. máx.
148.03 m
Altitude ejeção
198.65 m
Altitude aterragem
-2.04 m
Estabilidade
Pontuação estabilidade
86.1 / 100 (Excelente)
Inclinação no fim da queima (20%)93.3
Taxa arfagem/guinada (30%)93.7
Coning · boost (25%)77.9
Retidão de empuxo (15%)82
Launch tilt 2.6° · Coning 25.7/53.2°/s · Spin 452.2°/s · Thrust 96.2%
About this score
Worked out from the flight log between liftoff and 80% of apogee, independent of the angle the altimeter was mounted at in the airframe.
Inclinação no fim da queima (20%) – how close to vertical it left the rod.
Taxa arfagem/guinada (30%) and Coning · boost (25%) – how much the nose swung off the rocket's own axis. The main factor.
Retidão de empuxo (15%) – 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 line under the bars shows the raw measurements.
Velocidade
Máx. subida
156.91 m/s
Máx. descida
-14.88 m/s
No fim combustão
152.759 m/s
Vel. aterragem
-6.141 m/s
Vel. descida
-5.707 m/s
Vel. ejeção
144.82 m/s
Recovery
Single deploy (no dual deploy detected)
Aceleração
Máx. subida
31.02 G
Máx. descida
34.08 G
Máx. durante combustão
16.8 G
Média subida
1.25 G
Média combustão
11.64 G
Tempos
Fim combustão (primeiro)
1.41 seconds
Apogeu
11.42 seconds
Possível ejeção
1.863 seconds
Aterragem
129.3 seconds
Ângulos
Inclinação rampa
20.14°
Thrust calc pad tilt
2.6°
Incl. máx. até fim comb.
23.66°
Rolagem no lançamento
16.68°
Arfagem no lançamento
10.67°
Rotação máx. (comb.)
749.64 dps
Rotação média (comb.)
394.32 dps
Geral
Data envio
14/06/26-19:43:44
Amostras de dados
11536
Tempo total gravação
148.089 s
Média amostras/s
77.8
Número de bloqueios
0
Altitude gravação
42.09 m
Lançamento após arranque
7m 6s
Eixo de referência
X
Bateria & temperatura
Bateria início
88%
Bateria fim
82%
Temperatura início
28.38°C
Temperatura fim
30.12°C
Animação dos dados
FLIGHT 1786
756.68 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
Nota: A animação de voo requer que o altímetro esteja montado numa orientação fixa. Calibre os sensores para melhores resultados.
Notas do utilizador
A test of 2x Mercury and 2x Nano altimeters in a Lil Nuke with a G80 Aerotech motors.
Adicione este dispositivo à sua conta para editar
Vídeo Youtube
Sem vídeo
Adicione este dispositivo à sua conta para editar
Imagens do voo (0)
Sem imagens
Foguete associado
✅ Active
1
My Lil Nuke #1
LOC Precision — Lil' Nuke
✈️ 7 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
Sim data from sim files
| Motor | Alt | Vel | Accel | Apogee | Source |
|---|---|---|---|---|---|
| Estes A8-3 | 135.3 m | 64.8 m/s | 29.6 G | 4.5 s | RockSim (estes_viking.rkt) |
| Estes B4-4 | 282.9 m | 105.3 m/s | 30.0 G | 6.1 s | RockSim (estes_viking.rkt) |
| Estes B6-4 | 288.1 m | 116.9 m/s | 31.0 G | 5.9 s | RockSim (estes_viking.rkt) |
| Estes C6-5 | 475.1 m | 171.4 m/s | 34.4 G | 7.5 s | RockSim (estes_viking.rkt) |
| Estes C6-7 | 483.1 m | 171.4 m/s | 34.4 G | 8.1 s | RockSim (estes_viking.rkt) |
Informações do dispositivo
Nano V1
Este voo foi realizado num Nano V1.
Versão hardware
Rev 4
Versão software
1.52
Última ligação
14/06/26-19:43:44
Sensor pressão
Bosch BMP 581
Acelerómetro
32G 3-axis
Giroscópio
2000 dgps 3-axis
Motores do voo
1st Stage
1x
AeroTech
G80T-10
Burn time
1.70 seconds
Diameter
29.00 mm
Average thrust
77.60 N
Max thrust
108.50 N
Impulse
136.60 Ns
Impulse class
G
Total weight
127.90 g
Propellant weight
62.50 g
Propellant type
Blue Thunder
Links
Adicione este dispositivo à sua conta para editar
Combustão do motor
The dashed line is the combined thrust curve for your motors (data from thrustcurve.org), scaled so its peak matches the recorded acceleration maximum — the shape is meaningful, the absolute level is not (your rocket's weight is unknown).
Local de lançamento, data e hora
Clique no mapa para marcar o local de lançamento. Alterne entre vista de mapa e satélite.
No results found — try a different search.
Clique no mapa · Arraste para ajustar
Lat—
Lng—
✓ Launch location saved successfully.
✗ Could not save location — please try again.
Comparação de voo
Comparing against 3 other flights with the same motor configuration.
Highest apogee756.68 m 4th of 4
The maximum altitude reached above the launch point.
you
best
best 756.82 m · Lil Nuke - Flight with 4 altimeters - 1 (#1784)
Best stability86.1 /100 2nd of 4
How straight it flew: launch, coning and thrust straightness combined. 100 is perfect.
you
best
best 86.2 /100 · Lil Nuke - Flight with 4 altimeters - 4 (#1796)
Fastest velocity156.91 m/s 2nd of 4
Peak ascent velocity recorded during the flight.
you
best
best 159.41 m/s · Lil Nuke - Flight with 4 altimeters - 4 (#1796)
Best avg burn G3.36 G 4th of 4
Average acceleration during the motor burn, in G.
you
best
best 11.98 G · Lil Nuke - Flight with 4 altimeters - 1 (#1784)
Longest flight148.08 s 3rd of 4
Total recording time from launch to landing.
you
best
best 155 s · Lil Nuke - Flight with 4 altimeters - 1 (#1784)
Lowest spin394.32 dps 4th of 4
Average spin rate during the burn.
you
best
best 324.26 dps · Lil Nuke - Flight with 4 altimeters - 1 (#1784)
Coldest flight0.28 C 1st of 4
Board temperature at launch.
you
best
best 0.28 C · you
🌲 Is it in a tree?-2.04 m 2nd of 4
Just for fun: whichever flight came down closest to 8 m above the launch point (roughly tree height) is the one most likely stuck up a tree.
8 m
you
best
closest to 8 m · Lil Nuke - Flight with 4 altimeters - 4 (#1796) at -2.02 m
Definições gerais do voo
Este é um registo das definições utilizadas para este voo. Visite a
Visite a página Meus dispositivos e configure as definições..
Pressão prevista
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.
Xcweather.co.uk is a decent place to grab pressures from for your location and time.
1013.2 mbar
Deteção lançamento
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.
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 (50Hz)
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.
0
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).
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)
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.
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.
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.
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 1.0
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.
ATIVADO (24 samples / 140ms)
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.
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
Calibração de sensores
Desvios de calibração utilizados neste voo.
Giroscópio
X
2.000°
Y
0.000°
Z
0.000°
Acelerómetro
⚠ O acelerómetro não foi calibrado
X
0.000 mG
Y
0.000 mG
Z
0.000 mG
Comentários
Comentários
Iniciar sessão para comentar.
Iniciar sessão para comentar.