Bluetooth Rocket Launch Controller With Proximity Safety Checks

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Solution Overview

Problem

Existing model rocket launching systems face challenges in ensuring safe and controlled launches, often resulting in rockets landing far away and being lost due to lack of precise control and safety features.

Innovation Solution

A Bluetooth-enabled launch controller and mobile app system that includes safety features to prevent accidental launches, requires intentional user actions for launch initiation, and uses proximity detection, physical keys, and multiple confirmation steps to ensure safe operation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a simple electrical ignition system with remote control is used, then the device complexity is reduced, but the reliability and safety of launch control deteriorates

Engineering Contradiction:
Improveignition system complexityVSAvoidlaunch control safety
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The launch control system is divided into multiple independent safety modules: proximity detection module, physical key module, and confirmation sequence module. Each module performs a specific safety function and operates independently, preventing accidental launches while maintaining overall system reliability without excessive complexity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system performs preliminary safety checks before allowing launch: proximity detection is performed in advance, physical key insertion is required beforehand, and multiple confirmation steps must be completed prior to ignition. These preliminary actions ensure safety is established before the critical ignition event occurs.

Inventive Principle:
Principle #10Preliminary action

2Reliability

If multiple safety confirmation steps are implemented, then the reliability of launch control is improved, but the ease of operation deteriorates

Engineering Contradiction:
Improvelaunch control safetyVSAvoidlaunch initiation convenience
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The proximity detection system automatically detects the user's presence and enables/disables launch control without manual intervention. The physical key automatically authenticates the user when inserted. These self-service mechanisms handle safety checks automatically, reducing the operational burden on the user while maintaining high reliability.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

Multiple safety functions are merged into a single integrated launch controller that manages proximity detection, physical key authentication, and confirmation sequences through a unified interface. This consolidation presents a simplified operational workflow to the user while incorporating multiple safety layers in the background.

Inventive Principle:
Principle #5Merging (Combining)

3Object-affected harmful factors

If proximity detection and physical key requirements are added, then the safety against accidental launches is improved, but the device complexity increases

Engineering Contradiction:
Improveaccidental ignition riskVSAvoidcontrol system complexity
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

A physical key serves as an intermediary between the user and the launch control system. It provides a simple mechanical authentication mechanism that doesn't require complex electronics or programming, adding a layer of security against accidental launches while maintaining relatively simple implementation.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The system replaces complex electronic authentication mechanisms with simpler mechanical and optical solutions: proximity detection using optical sensors instead of complex electronic identifiers, and physical key insertion instead of electronic card readers or biometric scanners. This substitution reduces device complexity while maintaining safety.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

4Reliability

If a cloud-based tracking system is implemented, then the recovery capability of model rockets is improved, but the use of energy and device complexity increases

Engineering Contradiction:
Improverocket recovery capabilityVSAvoidenergy consumption
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

Instead of requiring continuous active communication and complex tracking hardware on the rocket, the system uses a simplified approach where the rocket transmits its identity and trajectory data briefly during flight, and the cloud system maintains a database copy of launch information. This reduces the energy requirements of the rocket while enabling comprehensive tracking and recovery capabilities.

Inventive Principle:
Principle #26Copying

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The system provides controlled and safe launches, reduces the risk of accidental ignition, and allows for tracking and data logging of rocket flights, enhancing user experience and recovery of model rockets.

Implementation Method 1

The launch controller (50) includes a Bluetooth® module (3600) that allows the launch controller (50) to wirelessly communicate with a mobile device

Methodology Applied
Scientific EffectBluetooth wireless communication: Electromagnetic Induction

Implementation Method 2

The launch controller (50) also includes a GPS receiver (3605) that allows the launch controller (50) to determine its own location

Methodology Applied
Scientific EffectGPS location tracking:

Implementation Method 3

In response to receiving a launch command from the mobile device, the igniter (102) ignites the engine (105)

Methodology Applied
Scientific EffectElectrical ignition: Joule Heating

Data Source

PatentUS20260034468A1Model rocket launching system
Publication Date: 2026.02.05 LANGFORD IND LLC
  • US20260034468A1 patent drawing
  • US20260034468A1 patent drawing
  • US20260034468A1 patent drawing

AI summary

A wireless model rocket launching system which provides for safety checking and advanced functionality to be performed wirelessly using a mobile communication device such as a cell phone. A set of safety checks can be performed before the rocket is armed and triggered for launch. In addition, a location of the rocket can be tracked wirelessly on the mobile communication device.