RC Airplane
Launcher
Precision Launch System for Consistent & Reliable Takeoffs
Overview
The RC Airplane Launcher is an innovative mechanical system designed to launch RC aircraft with precision, consistency, and safety. This project addresses the limitations of hand launches by providing a controlled takeoff mechanism suitable for various aircraft configurations.
Our launcher features adjustable launch angles, variable thrust settings, and a reliable release mechanism that ensures stable and predictable launches every time.
Why a Launcher?
Technical Specifications
Mechanical System
Performance
Control System
Portability
Development Timeline
Concept Development
Identified need for reliable launch system. Researched existing designs and analyzed requirements for our aircraft fleet.
Design Phase
Completed CAD modeling and structural analysis. Finalized mechanical design with focus on portability and ease of use.
Prototype Build
Fabricated first prototype using workshop facilities. Conducted initial tension and release mechanism tests.
Field Testing
Performed field tests with various aircraft models. Gathered data on launch consistency and reliability.
Optimization Phase
Refining design based on test results. Adding electronic controls and safety features for competition readiness.
Key Advantages
Consistent Launches
Eliminates variability of hand launches. Every takeoff is identical, perfect for testing and competitions.
Adjustable Settings
Customize launch parameters for different aircraft weights, wing loadings, and flight conditions.
Angle Control
Adjustable launch angle from 0-30° allows optimization for different aircraft types and weather conditions.
Safety First
Remote operation keeps pilot at safe distance. Automated checks prevent accidental launches and equipment damage.
Engineering Challenges
Challenge: Universal Mounting
Problem: Designing a mounting system compatible with aircraft of varying sizes and fuselage shapes.
✓ Solution: Created adjustable cradle system with padded clamps and quick-release mechanism. Accommodates fuselage diameters from 30mm to 100mm.
Challenge: Force Calibration
Problem: Determining optimal launch force for different aircraft weights without over-stressing airframes.
✓ Solution: Integrated load cell sensors and developed calibration protocol. Created lookup table for recommended settings based on aircraft specifications.
Project Gallery
