SP-1 Sharp Shinned: Solar Glider Concept

Mission Overview

The SP-1 is designed as an ultralight solar-assisted flying wing leveraging modern solar technologies for extended endurance. This isn't a weather reconnaissance jet — it's a sustainable flight platform focused on maximizing solar energy capture with minimal weight.

Key focus: Solar power-to-weight ratios, diamond wing geometry, and dual-seat ultralight operation with glider-level wing loading.

Design Parameters

• Wing Span: 15 m (optimal)
• Wing Area: ~80 m²
• Solar Power: 13.6 kW (modern)
• Solar Power: 29.6 kW (ultralight)
• Panel Weight: 152 kg / 40 kg
• Special Features: Solar-integrated wing, carbon fiber structure

Development Timeline

• 🟢
  Concept Phase: July 2025 – ongoing
  Includes solar power-to-weight analysis
• 🔜
  Structural Design: TBD
• 🔜
  Solar Array Integration: TBD
• 🔜
  Prototype Construction: TBD

Project Modules

• Aerodynamic Design
• Solar Array Integration
• Power Management
• Weight Optimization
• Propulsion System
• Research Documentation

Design Philosophy

• Geometry: Flying wing / diamond
• Solar Panels: Ultralight (500-750 W/kg)
• Operation: Single/Dual-seat ultralight
• Structure: Carbon fiber components
• Target: Feasible manufacturing

Technical Specifications

The SP-1 features a diamond wing planform inspired by the YF-23, optimized for maximum solar surface area and efficient aerodynamics.

• Endurance: Daylight unlimited (theoretical)
• Cruise Speed: 45-65 knots
• Payload: 1-2 operators + instruments
• Construction: Carbon fiber composite