VMAX Rocket

The VMAX Rocket is a thrust-vectoring model rocket inspired by SpaceX’s Raptor engine technology. Designed and built entirely by Liam Carlin, this project showcases advanced engineering techniques, including a two-axis gimbaling motor mount to maintain stable vertical ascent. The project bridges the gap between large-scale aerospace innovations and model-scale applications.

Overview Rocket Image

Thrust Vector Control (TVC) Mount

The Thrust Vector Control (TVC) Mount is the heart of the VMAX Rocket, enabling it to achieve stable and controlled flight without the need for traditional fins. Inspired by SpaceX’s gimbaling Raptor engine technology, this innovative system allows the rocket’s engine to pivot, keeping it on course during ascent.

What is a TVC Mount?

The TVC mount is a system that moves the rocket’s engine in two directions (X and Y axes), allowing the thrust to be directed dynamically. This control is essential for maintaining stability, especially in the absence of fins, by making real-time adjustments to counteract any disturbances during flight.

How It Works

  • Dynamic Control: The mount uses two small servo motors to tilt the engine based on data from onboard sensors.
  • Feedback Loop: A gyroscope and accelerometer provide real-time flight data, which is processed by a PID controller and Kalman filter. This ensures smooth and accurate corrections.
  • Above-Center Pivot Point: The mount’s pivot design maximizes stability and efficiency by placing the control point above the engine’s thrust center.

Design and Build

  • CAD-Designed: Fully modeled in Onshape, the mount was carefully engineered for precision.
  • 3D-Printed: Fabricated with high-grade PLA for strength and lightweight performance.
  • Integrated System: Works seamlessly with the rocket’s Arduino-based flight computer and sensors.

Why It Matters

  • No Fins Required: Traditional rockets rely on fins for stability, but the TVC mount eliminates this need, allowing for a sleeker design.
  • Real-Time Adjustments: The mount can instantly respond to external forces, such as wind or imbalance, ensuring a steady and vertical flight.
  • Advanced Control: This technology bridges the gap between professional aerospace systems and model rockets.

The VMAX Rocket’s TVC mount demonstrates how high-tech innovations can be applied on a smaller scale. It’s not just a model rocket feature—it’s a proof of concept for scalable, cutting-edge aerospace engineering.

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Technical Specifications

Arduino Uno

Arduino Uno
  • Microcontroller: ATmega328P
  • Operating Voltage: 5V
  • Digital I/O Pins: 14 (6 PWM outputs)
  • Analog Input Pins: 6
  • Clock Speed: 16 MHz
  • Usage: Central processor managing sensor data and controlling the gimbal system.

GY-521 MPU-6050 (Gyroscope + Accelerometer)

GY-521 MPU-6050
  • Axes: 3-axis gyroscope and 3-axis accelerometer combined.
  • Gyro Sensitivity Range: ±250, ±500, ±1000, ±2000 degrees/second.
  • Accelerometer Sensitivity Range: ±2g, ±4g, ±8g, ±16g.
  • Interface: I2C.
  • Operating Voltage: 3.3V-5V.
  • Usage: Measures both angular velocity and linear acceleration for flight stabilization.

BMP280 (Barometer)

BMP280
  • Pressure Range: 300-1100 hPa.
  • Accuracy: ±1 hPa.
  • Temperature Range: -40°C to +85°C.
  • Interface: I2C or SPI.
  • Usage: Tracks air pressure to estimate altitude during flight.

SG90 (Servo Motor)

SG90
  • Torque: 1.8 kg/cm (4.8V).
  • Speed: 0.1 sec/60° (4.8V).
  • Operating Voltage: 4.8V-6V.
  • Weight: 9g.
  • Usage: Controls the two-axis gimbal for precise thrust adjustments.

CANADUINO® Micro-SD Memory Card Adapter

CANADUINO® Micro-SD Memory Card Adapter
  • Supported Storage Capacity: Up to 32GB (FAT16/32 compatible).
  • Communication Protocol: SPI.
  • Operating Voltage: 3.3V-5V.
  • Usage: Logs flight data, including altitude, gimbal movements, and acceleration for post-flight analysis.

Estes F15 (Rocket Engine)

Estes F15
  • Thrust: 44.4 N.
  • Burn Time: 3.5 seconds.
  • Total Impulse: 80 N·s (F-class motor).
  • Dimensions: Diameter 24 mm, Length 95 mm.
  • Usage: Provides the main propulsion for the rocket with controlled thrust vectoring through the gimbal system.

Challenges and Solutions

Challenge: Imbalanced thrust due to flexible materials.

Imbalanced thrust

Solution: Upgraded to high-grade PLA for structural rigidity.

Challenge: Over-filtering in code led to delayed responses.

Over-filtering in code

Solution: Outsourced a refined Kalman filter implementation.

Challenge: Slow SD card writing caused data bottlenecks.

Slow SD card writing

Solution: Used a high-speed SD card and optimized data logging rates.

Next Steps

The VMAX Rocket will undergo additional MATLAB simulations to fine-tune its PID gains. The ultimate goal is to achieve:

  • Stable launch and recovery without parachutes.
  • Application of insights from VMAX to larger-scale rockets.

Further development will include:

  • Integration of advanced telemetry systems for real-time data monitoring.
  • Enhancement of the TVC mount for improved thrust vectoring accuracy.
  • Collaboration with aerospace experts to refine design and performance.
Next Steps Image

Call to Action

Interested in similar projects? Explore more of Liam Carlin’s work or reach out to collaborate!