Integrated Drone Propulsion Systems
Source integrated drone propulsion systems as complete matched configurations. Compare voltage, thrust conditions, rotation, propeller, mounting and interfaces using the X13 G2 reference.
| Reference configuration | Request quantity |
|---|---|
| X13 G2 — 18S system Unit: one propulsion system |
Images show the reference system. Rotation, delivery contents and packaging are quote-confirmed.
Integrated Drone Propulsion Systems for Complete Configuration Sourcing
Compare integrated drone propulsion systems as matched motor, ESC and propeller combinations. The current X13 G2 reference provides a starting point for 18S applications. Review voltage, thrust conditions, rotation, matched propeller, mounting and controller interfaces together before requesting a quotation.
Images illustrate the reference system. The delivered combination, cables, accessories and packaging are identified in the quotation; this page does not represent a standalone motor.
Reference Configuration and Quantity
| Configuration | System reference | Unit and status | Inquiry |
|---|---|---|---|
| X13 G2 — 18S system DN-IPS-X13-G2-18S |
18S LiPo reference; 69 V rated Integrated motor and system ESC; matched propeller specification |
One propulsion system Reference configuration; availability confirmed in quotation |
Add the reference to your Inquiry List and specify the number of propulsion units. State the required rotation allocation and spare-part quantities in your notes; one unit is not a complete multi-axis aircraft set.
System Technical Reference
| Recommended battery / rated voltage | 18S LiPo / 69 V |
|---|---|
| Input voltage range | 25–80 V |
| Sea-level thrust reference | 60 kg maximum thrust per axis; 27 kg recommended takeoff weight per axis |
| Rated output power | 2700 W maximum continuous |
| Motor reference | 45 KV; 36N42P; stator 138 × 25 mm; motor diameter 148 mm |
| Integrated ESC reference | 18S; 70 A continuous; 200 A peak for 3 s; Cyphal (UAVCAN); PWM + CAN throttle |
| Default propeller specification | MFP 56×20 folding; actual delivery version confirmed in quotation |
| Mounting tube reference | D50 mm |
| Environment reference | −20 to 50 °C; IPX6 |
| Reference mass and cables | 4185 g with cable and propeller; power cable 10 AWG / 1355 mm; signal cable 1120 mm |
Thrust, efficiency and current depend on the matched propeller, voltage, atmosphere, load and test conditions. Use the performance record for the quoted configuration; do not combine maxima from different tests. IPX6 does not establish immersion protection.
Aircraft and Controller Integration
Provide aircraft takeoff weight, number of axes, battery, required thrust/duty profile, installation envelope, tube and mounting interface, rotation direction and flight-controller support. Confirm controller protocol, firmware, signal harness, connectors and cable routing. A separately listed 14S ESC is not established as a replacement for this integrated 18S system.
Included Items and Accessory Checklist
- Confirm the complete delivered motor, system ESC, matched propeller and cable set.
- Specify rotation direction, propeller version and spare blades/propellers separately.
- Confirm mounting parts, fasteners, protective covers and configuration equipment if required.
- Battery, aircraft frame, other propulsion axes and flight controller are not assumed included.
- Identify unit packaging, labels, documentation and carton quantity in the packing list.
Need a Different Propulsion Configuration?
Submit a system requirement with supply voltage, takeoff weight, thrust and duty conditions, matched combination if known, rotation allocation, mounting drawing, interfaces, environmental conditions, quantity and destination. Other systems or changes require complete configuration and feasibility review. Motors, ESCs and propellers are not freely interchangeable catalog options.
MOQ, Samples and Lead Time
Include sample and bulk quantities and the required date. Supply, minimum quantities, sample arrangements, price and dispatch schedule are confirmed for the complete proposed configuration. Sampling or modification work and transportation are addressed separately.
Inspection, Documentation and Repeat Orders
Agree component identities and revisions, rotation, propeller, cable termination, mounting and protocol checks before ordering. Define functional and performance checks with their operating conditions. For repeat orders, provide the previous system code, order reference or label photos. Retain labels and test records for any issue review against the agreed specification.
Integrated Propulsion System FAQ
Is this a standalone motor?
No. The reference is an integrated propulsion system and must be evaluated as a complete combination.
Can I choose any listed propeller or ESC?
No. Confirm the matched system and version before quotation; a requested substitution needs its own review.
How do I request several rotation directions?
State each direction and its quantity in the inquiry notes so the proposed system allocation is explicit.
Browse propulsion references or the products directory for related procurement requests.
| Reference configuration | X13 G2 — 18S system |
|---|
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