Practical, engineering-led guidance on selecting and sourcing propulsion for high-speed UAVs and target drones — written by the Sheng-Fang engineering team.
Speed, fuel burn, weight, altitude, cost and mission fit — a propulsion engineer's framework for matching the engine class to the platform.
Read guide → Engine SelectionThrust-to-weight, envelope, life cycle and export requirements for 400 kgf (4,000 N) class turbojets powering target drones and large UAVs.
Read guide → Engine ComparisonA side-by-side engineering comparison of 1,000-4,200 N turbojets for platforms that have outgrown the PBS TJ100 thrust range.
Read guide → Export ComplianceDual-use thresholds, licensing timelines and the documents needed to import high-thrust UAV turbojets without program delays.
Read guide →