Turbojet Engines: Model & Specification Selection
Turbojet engines for UAV and test applications. Compare published thrust and conditions, fuel, power, interface and supply scope model by model.
How to compare turbojet engines
Compare published thrust in its original unit and condition; do not convert daN to kg or compare headline numbers without the test condition.
- Thrust and condition: published thrust at ISA and the associated speed or altitude condition; confirm the exact model and test basis.
- Fuel and power: fuel type, consumption, supply and starting power; confirm the project installation.
- Interface and installation: mounting, connectors, control and telemetry; confirm the airframe or test stand.
- Supply scope: included accessories, spares and documentation; request the configuration list.
Send the model, required thrust condition, installation and destination for a quotation.
AT-TP100 Turbojet Engine
95 daN variant of the 202 mm AT-TP class at 11.5 kg and 508 mm length, moving 1.6 kg/s of air at up to 64,000 rpm and burning 2.95
AT-TP100S Turbojet Engine
Longer 560 mm variant of the 202 mm AT-TP class: 92 daN at ISA from 12.5 kg, with the family's raised 4,500 m maximum starting alt
AT-TP125 Turbojet Engine
125 daN turbojet at 16.5 kg in a 234 × 568 mm envelope, improving SFC to 1.38 kg/daN·h with 3.7 L/min fuel use and 2.0 kg/s mass f
AT-TP160 Turbojet Engine
158 daN at ISA from a 22.5 kg, 261 × 646 mm unit with 2.7 kg/s mass flow, 20,000 rpm idle speed and a 780 °C maximum exhaust gas t
AT-TP220 Turbojet Engine
Top of the AT-TP range: 220 daN at ISA from 27 kg and 248 × 769 mm, with the family's highest ceilings — starting to 6,000 m and f
AT-TP40 Turbojet Engine
Entry-class turbojet in the AT-TP family: 41 daN of thrust at ISA from a 3.8 kg, 147.6 × 342 mm unit that starts up to 4,000 m and
AT-TP40 Pro Turbojet Engine
Higher-output variant of the 40-class turbojet: 45 daN at ISA from the same 147.6 mm diameter envelope at 3.9 kg, running to 96,00
AT-TP60 Turbojet Engine
Mid-range AT-TP turbojet rated 59 daN at ISA, 5.8 kg in a 174 × 410 mm envelope, moving 1.0 kg/s of air at up to 78,000 rpm for co
AT-TP60 Pro Turbojet Engine
65 daN variant of the 174 mm AT-TP class at 5.9 kg and 435 mm length, delivering 1.12 kg/s mass flow at 81,000 rpm maximum speed a
AT-TP80 Turbojet Engine
80 daN turbojet at 11 kg in a 202 × 502 mm envelope, starting to 4,000 m and flying to 12,000 m, with 1.35 kg/s mass flow and a 25
Listings in this category show EXW tier pricing at 5, 20 and 50 units where available, with MOQ and packing details on each product page. Need a configuration that is not listed? Request a quotation — pricing is valid for 14 days and OEM configurations are available.
Frequently Asked Questions
What does Aerosys Technology supply?
Our catalogue covers 279 product models across 13 categories. Behind that catalogue sits production in the Pearl River Delta and a commercial centre in Hong Kong that handles the contracting, freight, banking and export documentation cross-border trade depends on.
What is the minimum order quantity?
It depends on the product line. Ground control stations are quoted on a 5-unit basis, while video and data links and camera payloads are quoted from a single unit. Complete platforms such as VTOL aircraft, multi-rotors and unmanned ground vehicles are quoted per set. Where a product page states a different MOQ, that page governs.
How do I get a quotation, and how long is it valid?
Send us the model numbers and quantities you need by email. Quotations are issued in USD and are valid for 14 days from the date of issue unless a different period is stated. An order is confirmed only when we issue a written order confirmation and receive the agreed payment; a quotation or an email alone is not an accepted order.