Heritage Meets Innovation
From dusty runways to orbital operations—the Shinar-67 family carries forward DC-3 DNA with 21st century capability.
"Classic airframe. Modern mission systems. Unlimited capability."
Next-generation aircraft platforms and sovereign orbital infrastructure
From dusty runways to orbital operations—the Shinar-67 family carries forward DC-3 DNA with 21st century capability.
"Classic airframe. Modern mission systems. Unlimited capability."
Built on DC-3 heritage with modern engineering. Modular, field-repairable, and mission-adaptable for NGO, cargo, VIP, and specialized operations.
Foundation variant with PT6A-65B engines, tundra gear, and rugged field capability.
Regional workhorse with +1.0m plug, PT6A-67R, and modular cargo systems.
+4.7m total stretch with flat cargo deck, rear ramp, and mission-specific kits.
High-performance variant with GE Catalyst engines, laminar wing, and semi-retract gear.
Extended-range executive transport with tip tanks, dual FADEC, and premium systems.
Ultimate executive platform with VIP seating, dual WC, and localized O₂ enrichment.
Fully electric variant with 150 kWh battery, ultralight configuration, and ~5hr charge.
Long-endurance orbital control aircraft with mission bay, C2 rack, and dual SATCOM.
Air-launch carrier for 2.8t orbital rockets via underbelly cradle at 12-14k ft AGL.
Modular sovereign orbital infrastructure-as-a-service. Hot-swappable nodes, open API, and corridor-based manufacturing for democratized space access.
Shinar-67 Speed+ Launcher carries 2.8t micro-rockets to 12–14k ft AGL, then releases for orbital insertion
Tier 1 partners (SpaceX, etc.) for larger payloads and initial station deployment
Air-launch from austere airfields enables flexible launch windows and reduced infrastructure costs. Micro-launcher approach allows rapid node deployment and replacement.
Foundational microstation with modular nodes, passive clamp rings, and shared power/data bus. Designed for 500-600 km LEO.
Ion/Hall effect propulsion for station-keeping and inclination tuning. 3-5 year coverage with autonomous mode + API fallback.
Partner satellite interface accepting 1U-12U payloads. Open SDK for university/NGO clients with API-exposed services.
Lifecycle management with time-tagged modules. AI-tracked health monitoring and automated swap priority at 5-10% EOL.
Distributed orbital operations layer. Stations broadcast availability, health, and form regional orbital mesh dynamically.
Corridor-based integration with modules manufactured in Tier 2.5 nations. GitHub-style shared evolution of hardware & software.
Tool-free maintenance with DZUS panels, QR diagnostics, and field-swappable systems. Village-hangar capable.
FAA Part 25 compliance with phased certification across variants. Part 135/121 operational support.
Garmin G3X suite with EFB integration, STOL presets, and field-swappable LRU architecture.
ITAR-light eligible, NGO-ready, with modular export configurations and multi-language support.
Speed+ Launcher variant enables micro-rocket deployment to LEO from austere airfields.
Houston-A provides 6-9hr loiter for Sky-Star C2, telemetry, and mission coordination.
Partner with us to deploy modular aviation and orbital infrastructure solutions tailored to your mission.