Low-altitude aircraft

Plastic materials for consumer and industrial drones

All materials · 11 grades

Parts and materials of the quadcopter drone

Pain points and material advice

  • Lightweighting and stiffness

    Pain point
    The heavier the arms and body, the shorter the flight time. Arms that are not stiff enough cause vibration, which affects flight control and imaging.
    Advice
    Screen materials by specific stiffness. Carbon-fiber-reinforced PA has about half the density of aluminum alloy. Fiber orientation should follow the main load direction of the arm. Validate folding joints for fatigue and drop.
  • Battery bay safety

    Pain point
    Drone batteries have high energy density and high charge and discharge currents. Battery housings and areas around the battery compartment need flame retardancy and must not produce drips when burning.
    Advice
    Use halogen-free flame-retardant PC/ABS or PC for battery housings and test UL 94 at the actual wall thickness. Snap fits on plug-in batteries must balance toughness and wear resistance. For models used in winter, run low-temperature impact tests.
  • Signal transmission

    Pain point
    Video transmission, remote control, GNSS and RTK antennas all need signals to pass freely. Carbon fiber materials block signals.
    Advice
    Use non-conductive materials such as PC, ASA or PC/ASA for radomes and around antennas. Avoid metallic-effect pigments. Measure dielectric constant and loss where needed.
  • Outdoor exposure: cold, UV and chemicals

    Pain point
    Drones work at altitude and in winter, at low temperatures. Long sun exposure fades housings and makes them brittle. Crop protection drones also come into contact with pesticides.
    Advice
    Choose weather-resistant grades for appearance parts and test impact and color difference after xenon-arc weathering. Test crop protection parts for chemical resistance with the actual agents. Set the low-temperature impact temperature by the flight environment.
  • Fast development, many models

    Pain point
    Drone models change fast, and industrial models come in small batches with much customization.
    Advice
    At the prototype stage, 3D print arms and brackets in carbon fiber PA filament for assembly and flight validation. For mass production, switch to injection molding with the equivalent pellets. Printed part properties are directional, so validate again with molded parts before mass production.

Material selection for airframes, arms, propellers, landing gear, gimbals, battery bays, motor mounts, antenna covers, connectors and payload pods in consumer, industrial, agricultural and cargo drones.

Materials in the quadcopter drone

Example grade / typical values — to be corrected by GREENPOLYMER Typical values. Refer to the actual TDS.

  • GRN-PA6-C310

    Carbon-fiber-reinforced PA6 (CFRPA)

    Tensile strengthISO 527-1/-2 · dry
    180–250 MPa
    Flexural modulusISO 178
    13–20 GPa
    Heat deflection temperatureISO 75-1/-2 · 1.80 MPa
    200–215 °C
    MoreLess

    Features

    Light, stiff, fatigue-resistant

    Typical values

    Charpy notched impact strengthISO 179-1/1eA · 23 °C; dry
    8–14 kJ/m²
    DensityISO 1183
    1.20–1.28 g/cm³
    Flammability ratingUL 94 · 1.5 mm; design target, subject to test report
    HB

    Processing

    Drying
    80 °C, 4–6 h (desiccant dryer); moisture content 0.05–0.2 % recommended
    Melt temperature
    260–290 °C
    Mold temperature
    80–100 °C; upper end for a better surface

    Why this material

    • Arms (incl. folding arms)Light and stiff; folding structures can be molded in one shot
    • Body shell / center frameCarries the battery, flight controller and gimbal; high appearance requirements for consumer models
    • PropellersMust stay stiff and keep its shape at high speed; injection molding for volume production
    • Gimbal parts, camera housingLight and stiff to reduce shake; good appearance
  • GRN-PCA-W310

    Weather-resistant PC/ABS

    Tensile strengthISO 527-1/-2
    50–58 MPa
    Weathering (color difference)ISO 4892-2 · Xenon-arc 1000 h; design target
    ΔE ≤ 3
    Charpy notched impact strengthISO 179-1/1eA · 23 °C
    35–55 kJ/m²
    MoreLess

    Features

    UV-resistant, color-stable outdoors

    Typical values

    Heat deflection temperatureISO 75-1/-2 · 1.80 MPa
    95–110 °C
    DensityISO 1183
    1.12–1.16 g/cm³
    Flammability ratingUL 94 · 1.5 mm; design target, subject to test report
    HB

    Processing

    Drying
    100–110 °C, 3–4 h
    Melt temperature
    250–280 °C
    Mold temperature
    60–90 °C

    Why this material

    • Carries the battery, flight controller and gimbal; high appearance requirements for consumer models
  • GRN-PA6-E510

    Flame-retardant glass-fiber-reinforced PA6 (GFRPA)

    Tensile strengthISO 527-1/-2 · dry
    130–160 MPa
    Flammability ratingUL 94 · 1.5 mm; design target, subject to test report
    V-0
    Flexural modulusISO 178
    8–10 GPa
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    Features

    Stiff, fatigue-resistant, wear-resistant

    Typical values

    Heat deflection temperatureISO 75-1/-2 · 1.80 MPa
    190–205 °C
    Charpy notched impact strengthISO 179-1/1eA · 23 °C; dry
    8–12 kJ/m²
    DensityISO 1183
    1.40–1.50 g/cm³

    Processing

    Drying
    80 °C, 4–6 h (desiccant dryer); moisture content 0.05–0.2 % recommended
    Melt temperature
    260–290 °C
    Mold temperature
    80–100 °C; upper end for a better surface

    Why this material

    • Takeoff and landing impacts; light weight; doubles as an antenna mount on some models
  • GRN-PC-L110

    Transparent PC

    Tensile strengthISO 527-1/-2
    60–68 MPa
    Light transmittanceISO 13468-1 · 3 mm; design target
    ≥ 88 %
    Charpy notched impact strengthISO 179-1/1eA · 23 °C
    60–80 kJ/m²
    MoreLess

    Features

    Light-transmitting, impact-resistant

    Typical values

    Heat deflection temperatureISO 75-1/-2 · 1.80 MPa
    125–135 °C
    DensityISO 1183
    1.19–1.21 g/cm³
    Flammability ratingUL 94 · 1.5 mm; design target, subject to test report
    HB

    Processing

    Drying
    120 °C, 3–4 h; moisture content ≤ 0.02 % recommended
    Melt temperature
    280–310 °C; for flame-retardant grades keep within the TDS upper limit
    Mold temperature
    80–110 °C

    Why this material

    • Light and stiff to reduce shake; good appearance
  • GRN-PC-L120

    IR-transmissive black PC

    Tensile strengthISO 527-1/-2
    60–68 MPa
    Charpy notched impact strengthISO 179-1/1eA · 23 °C
    60–80 kJ/m²
    Heat deflection temperatureISO 75-1/-2 · 1.80 MPa
    125–135 °C
    MoreLess

    Features

    Black, IR-transmissive

    Typical values

    DensityISO 1183
    1.19–1.21 g/cm³
    Flammability ratingUL 94 · 1.5 mm; design target, subject to test report
    HB

    Processing

    Drying
    120 °C, 3–4 h; moisture content ≤ 0.02 % recommended
    Melt temperature
    280–310 °C; for flame-retardant grades keep within the TDS upper limit
    Mold temperature
    80–110 °C

    Why this material

    • Light and stiff to reduce shake; good appearance
  • GRN-PCA-H320

    Low-temperature high-impact PC/ABS

    Tensile strengthISO 527-1/-2
    48–56 MPa
    Charpy notched impact strengthISO 179-1/1eA · 23 °C; −30 °C: 25–40 kJ/m²
    45–65 kJ/m²
    Heat deflection temperatureISO 75-1/-2 · 1.80 MPa
    95–110 °C
    MoreLess

    Features

    Good appearance, low-temperature toughness

    Typical values

    DensityISO 1183
    1.12–1.15 g/cm³
    Flammability ratingUL 94 · 1.5 mm; design target, subject to test report
    HB

    Processing

    Drying
    100–110 °C, 3–4 h
    Melt temperature
    250–280 °C
    Mold temperature
    60–90 °C

    Why this material

    • Light and stiff to reduce shake; good appearance
  • GRN-PCA-N510

    Halogen-free flame-retardant PC/ABS

    Tensile strengthISO 527-1/-2
    55–65 MPa
    Flammability ratingUL 94 · 1.5 mm; design target, subject to test report
    V-0
    Charpy notched impact strengthISO 179-1/1eA · 23 °C
    10–30 kJ/m²
    MoreLess

    Features

    Halogen-free, flame-retardant

    Typical values

    Heat deflection temperatureISO 75-1/-2 · 1.80 MPa
    80–95 °C
    DensityISO 1183
    1.17–1.20 g/cm³

    Processing

    Drying
    100–110 °C, 3–4 h
    Melt temperature
    250–280 °C
    Mold temperature
    60–90 °C

    Why this material

    • Flame retardancy around the lithium battery; plug-in batteries must be wear and impact resistant
  • GRN-PA6-C510

    Flame-retardant carbon-fiber-reinforced PA6 (CFRPA)

    Tensile strengthISO 527-1/-2 · dry
    160–220 MPa
    Flammability ratingUL 94 · 1.5 mm; design target, subject to test report
    V-0
    Flexural modulusISO 178
    12–18 GPa

    Used for

    MoreLess

    Features

    Stiff, heat-resistant, creep-resistant

    Typical values

    Heat deflection temperatureISO 75-1/-2 · 1.80 MPa
    190–210 °C
    Charpy notched impact strengthISO 179-1/1eA · 23 °C; dry
    6–10 kJ/m²
    DensityISO 1183
    1.25–1.35 g/cm³

    Processing

    Drying
    80 °C, 4–6 h (desiccant dryer); moisture content 0.05–0.2 % recommended
    Melt temperature
    260–290 °C
    Mold temperature
    80–100 °C; upper end for a better surface

    Why this material

    • Motor vibration and heat; needs stiffness and heat resistance
  • GRN-PCAS-W310

    Weather-resistant PC/ASA

    Tensile strengthISO 527-1/-2
    50–60 MPa
    Weathering (color difference)ISO 4892-2 · Xenon-arc 1000 h; design target
    ΔE ≤ 3
    Charpy notched impact strengthISO 179-1/1eA · 23 °C
    30–50 kJ/m²
    MoreLess

    Features

    Weather-resistant, impact-resistant, low loss

    Typical values

    Heat deflection temperatureISO 75-1/-2 · 1.80 MPa
    95–110 °C
    DensityISO 1183
    1.14–1.17 g/cm³
    Flammability ratingUL 94 · 1.5 mm; design target, subject to test report
    HB

    Processing

    Drying
    80–85 °C, 2–4 h
    Melt temperature
    230–260 °C
    Mold temperature
    50–80 °C

    Why this material

    • Must let wireless signals through; outdoor weather resistance
  • GRN-PA66-E510

    Halogen-free flame-retardant glass-fiber-reinforced PA66

    Tensile strengthISO 527-1/-2 · dry
    140–170 MPa
    Flammability ratingUL 94 · 1.5 mm; design target, subject to test report
    V-0
    Flexural modulusISO 178
    8–10 GPa
    MoreLess

    Features

    Heat-resistant, dimensionally accurate, halogen-free flame-retardant

    Typical values

    Heat deflection temperatureISO 75-1/-2 · 1.80 MPa
    230–250 °C
    Charpy notched impact strengthISO 179-1/1eA · 23 °C; dry
    8–12 kJ/m²
    DensityISO 1183
    1.45–1.55 g/cm³

    Processing

    Drying
    80 °C, 4–6 h (desiccant dryer); moisture content 0.05–0.2 % recommended
    Melt temperature
    280–300 °C; do not exceed the TDS upper limit for flame-retardant grades
    Mold temperature
    80–110 °C

    Why this material

    • High current; plugging and unplugging; close to hot components
  • GRN-PP-E510

    Flame-retardant glass-fiber-reinforced PP

    Tensile strengthISO 527-1/-2
    50–70 MPa
    Flammability ratingUL 94 · 1.5 mm; design target, subject to test report
    V-0
    Flexural modulusISO 178
    4–6 GPa
    MoreLess

    Features

    Chemical-resistant, stiff

    Typical values

    Heat deflection temperatureISO 75-1/-2 · 1.80 MPa
    120–145 °C
    Charpy notched impact strengthISO 179-1/1eA · 23 °C
    5–9 kJ/m²
    DensityISO 1183
    1.15–1.30 g/cm³

    Processing

    Drying
    Usually not needed; if damp, 80 °C, 1–2 h
    Melt temperature
    190–220 °C (not too high for flame-retardant grades)
    Mold temperature
    30–60 °C

    Why this material

    • Contact with pesticides and water; needs chemical and impact resistance

Industry overview and trends

  • Drone numbers are growing fast

    By the end of 2025, about 3.287 million drones were registered in China, up about 51 % on the previous year. In 2025 drones flew about 45.3 million hours in total, up about 70 %.

  • Industrial drones make up the larger share

    In 2025, China's civil drone output was worth about RMB 176.1 billion, up about 20 %. Industrial drones accounted for about RMB 125.9 billion and consumer drones about RMB 50.2 billion. Inspection, surveying, crop protection, emergency response and logistics are the main uses.

  • The low-altitude economy is scaling up

    Low-altitude flight service stations, vertiports and routes are being built across the country. Logistics delivery, urban inspection, tourism and other uses are moving from pilots to regular operation. Import and export trade in unmanned aircraft was about RMB 23.3 billion, up about 44 %.

  • Safety requirements are more specific

    Safety requirements for civil unmanned aircraft systems are in force as a mandatory national standard (GB 42590-2023, fully applied from 2024-06-01). It sets requirements on structural strength, batteries, electromagnetic compatibility, remote identification and more. The standard applies to the complete aircraft, and materials must leave the aircraft margin to pass its tests.

  • Lightweighting and reliability at the same time

    Every bit of weight saved on the airframe helps flight time and payload. Industrial drones fly longer and carry heavier loads, and must also withstand low temperatures, UV, pesticides and humidity. Using carbon- and glass-fiber-reinforced plastics for arms and body frames is typical industry practice.

  • Drones flew about 45.3 million hours in 2025 (about +70 %).
  • In 2025, the output value of civil drones in China was about RMB 176.1 billion (about +20 %): industrial drones about RMB 125.9 billion, consumer drones about RMB 50.2 billion.
  • The low-altitude economy is scaling up: flight service stations, landing sites and routes are being built. Drone import and export trade reached about RMB 23.3 billion (about +44 %).
  • GB 42590-2023, the mandatory national safety standard for civil unmanned aircraft systems, has been fully in force since 2024-06-01.

Part-to-material guide

Full list · 13 parts

This table shows common industry practice for first-round selection. The final choice depends on the applicable standards, load analysis and validation results (to be verified by GREENPOLYMER).

Arms (incl. folding arms)

Typical materials: Carbon-fiber-reinforced PA6 / PA66, glass-fiber-reinforced PA, carbon fiber tubes + plastic joints
Why

Light and stiff; folding structures can be molded in one shot

Key requirements

Specific stiffness (vibration control); fatigue resistance; drop impact; low-temperature toughness

Common standards

ISO 527; ISO 178; ISO 179; fatigue and vibration tested on the complete aircraft

GREENPOLYMER grade

GRN-PA6-C310 (carbon fiber, non-flame-retardant); GRN-PA6-C510 (flame-retardant carbon fiber)

Example grade / typical values — to be corrected by GREENPOLYMER

Body shell / center frame

Typical materials: Carbon or glass-fiber-reinforced PA, PC/ABS (consumer housings), PC
Why

Carries the battery, flight controller and gimbal; high appearance requirements for consumer models

Key requirements

Stiffness; dimensional stability; appearance; low-temperature impact; UV resistance

Common standards

ISO 178; ISO 179; GB 42590-2023 clause 4.4 structural strength and clause 4.6 drop, both tested on the complete aircraft

GREENPOLYMER grade

Structure: GRN-PA6-C310, GRN-PA6-E510; housings: GRN-PCA-H320, GRN-PCA-W310

Example grade / typical values — to be corrected by GREENPOLYMER

Propellers

Typical materials: Glass or carbon-fiber-reinforced PA6 / PA66; carbon fiber composites for large aircraft
Why

Must stay stiff and keep its shape at high speed; injection molding for volume production

Key requirements

Stiffness and dynamic balance; fatigue resistance; no sharp fragments after impact; consistent dimensions

Common standards

GB 42590-2023 clause 4.5.2: micro and light models without propeller guards must not use metal propellers; dynamic balance and burst speed per customer testing

GREENPOLYMER grade

Small propellers: GRN-PA6-C310. Non-flame-retardant high-toughness glass fiber PA: Available as a project-based development

Example grade / typical values — to be corrected by GREENPOLYMER

Landing gear / skids

Typical materials: Glass-fiber-reinforced PA, PC/ABS, PA + TPU feet
Why

Takeoff and landing impacts; light weight; doubles as an antenna mount on some models

Key requirements

Impact (including low temperature); fatigue resistance; wear resistance

Common standards

ISO 179; GB 42590-2023 clause 4.6 drop, tested on the complete aircraft

GREENPOLYMER grade

GRN-PA6-E510; GRN-PCA-H320; TPU for feet: Available as a project-based development

Example grade / typical values — to be corrected by GREENPOLYMER

Gimbal parts, camera housing

Typical materials: Carbon-fiber-reinforced PA, PC/ABS, PC; transparent PC or glass for lens protectors
Why

Light and stiff to reduce shake; good appearance

Key requirements

Dimensional accuracy; stiffness; low-temperature toughness; light transmission and scratch resistance of the lens protector

Common standards

ISO 178; ISO 13468 (transparent parts); IEC 60529

GREENPOLYMER grade

GRN-PA6-C310; GRN-PCA-H320; transparent parts: GRN-PC-L110. Obstacle avoidance and ranging sensor windows: IR-transmissive black PC is available for sensor and LiDAR windows

Example grade / typical values — to be corrected by GREENPOLYMER

Battery housing / battery bay

Typical materials: Flame-retardant PC/ABS, flame-retardant PC; flame-retardant reinforced PA for industrial models
Why

Flame retardancy around the lithium battery; plug-in batteries must be wear and impact resistant

Key requirements

Flame retardancy, rating per the OEM's specification and assessed at the actual wall thickness; halogen-free; impact (including low temperature); dimensional stability

Common standards

UL 94; IEC 62133-2; UN 38.3 (transport, the battery itself)

GREENPOLYMER grade

GRN-PCA-N510; GRN-PC-N510; GRN-PCA-S520 (halogen-free, without PTFE anti-drip agent); structural parts: GRN-PA6-C510

Example grade / typical values — to be corrected by GREENPOLYMER

Motor mounts

Typical materials: Carbon or glass-fiber-reinforced PA6 / PA66, aluminum alloy (heavy payloads)
Why

Motor vibration and heat; needs stiffness and heat resistance

Key requirements

Stiffness; heat resistance (motor temperature rise); creep resistance (screw clamping)

Common standards

ISO 75; ISO 178

GREENPOLYMER grade

GRN-PA6-C510; GRN-PA66-E510 (halogen-free flame retardant)

Example grade / typical values — to be corrected by GREENPOLYMER

Antenna covers / RTK and video-link antenna housings

Typical materials: PC, ASA, PC/ASA, glass-fiber-reinforced PBT; no carbon fiber
Why

Must let wireless signals through; outdoor weather resistance

Key requirements

Low dielectric constant and loss; UV resistance; impact resistance

Common standards

Dielectric properties per customer specification; IEC 60529

GREENPOLYMER grade

GRN-PCAS-W310; GRN-ASA-W110; GRN-PC-L110 (transparent cover)

Example grade / typical values — to be corrected by GREENPOLYMER

Connectors, ESC and power-board brackets

Typical materials: Flame-retardant glass-fiber-reinforced PA66, PBT-GF
Why

High current; plugging and unplugging; close to hot components

Key requirements

V-0; comparative tracking index (CTI); heat resistance; dimensional accuracy

Common standards

UL 94; IEC 60112; IEC 60695-2-12 / -13

GREENPOLYMER grade

GRN-PA66-E510; GRN-PBT-E510 (high CTI)

Example grade / typical values — to be corrected by GREENPOLYMER

Payload pods, mission-payload housings

Typical materials: Glass-fiber-reinforced PC/ABS, carbon-fiber-reinforced PA, weather-resistant PC/ASA
Why

Carries LiDAR, spraying, lighting and other payloads; often needs quick release

Key requirements

Stiffness; UV resistance; chemical resistance (pesticides); IP protection

Common standards

IEC 60529; chemical resistance tested with the actual media

Example grade / typical values — to be corrected by GREENPOLYMER

Spray tank and spray parts (agricultural)

Typical materials: PE, PP, glass-fiber-reinforced PP, PA
Why

Contact with pesticides and water; needs chemical and impact resistance

Key requirements

Chemical resistance; UV resistance; drop impact; low-temperature toughness

Common standards

Chemical resistance tested with the actual agents

GREENPOLYMER grade

Reinforced parts: GRN-PP-E510 (flame retardant). Non-flame-retardant chemical-resistant PP: Available as a project-based development

Example grade / typical values — to be corrected by GREENPOLYMER

Cargo box / cargo-bay housing

Typical materials: PC/ABS, PP, weather-resistant PC/ASA, glass-fiber-reinforced PA (frame)
Why

Large and light; outdoor use; often works with food delivery or parcel lockers

Key requirements

Light weight; impact; UV resistance; dimensional stability

Common standards

ISO 179; weather resistance to ISO 4892-2

GREENPOLYMER grade

GRN-PCAS-W310; GRN-PCA-W310; frame: GRN-PA6-E510

Example grade / typical values — to be corrected by GREENPOLYMER

Remote controller / ground-station housing

Typical materials: PC/ABS, ABS, PC; flame retardant when a lithium battery is built in
Why

Handheld, so appearance and feel matter; outdoor use

Key requirements

Impact; appearance; UV resistance; flame retardancy (with a built-in battery)

Common standards

UL 94; IEC 62368-1

GREENPOLYMER grade

GRN-PCA-H320; GRN-PCA-N510 (flame retardant); GRN-PCA-W310

Example grade / typical values — to be corrected by GREENPOLYMER

Notes

  • Carbon-fiber-reinforced materials may conduct electricity and may block signals. Do not use carbon fiber materials for radomes, near GPS/RTK antennas or in video transmission areas unless validated.
  • Nylon absorbs moisture. Conditioned strength and modulus are lower than the dry values. Check arms and propellers in their actual service condition.
  • Temperatures are low at altitude and in winter. Set the low-temperature impact test temperature by the flight environment (such as −20 °C, −30 °C).
  • GB 42590-2023, EU Delegated Regulation (EU) 2019/945 (drone product requirements, currently in force) and similar are aircraft-level standards; they apply to the complete aircraft, not to the material itself.

GREENPOLYMER grades for low-altitude aircraft

GradeMaterialRecommended partsDensityTensileNotched impactFlammability (target)
GRN-PA6-C310Carbon-fiber-reinforced PA6 (non-flame-retardant)Arms, airframes, gimbals, small propellers1.20–1.28 g/cm³180–250 MPa (dry)8–14 kJ/m² (dry)HB @ 1.5 mm
GRN-PA6-C510Flame-retardant carbon-fiber-reinforced PA6Battery compartment structures, motor mounts1.25–1.35 g/cm³160–220 MPa (dry)6–10 kJ/m² (dry)V-0 @ 1.5 mm
GRN-PA6-E510Flame-retardant glass-fiber-reinforced PA6Landing gear, brackets, cargo box frames1.40–1.50 g/cm³130–160 MPa (dry)8–12 kJ/m² (dry)V-0 @ 1.5 mm
GRN-PA66-E510Halogen-free flame-retardant glass-fiber-reinforced PA66Motor mounts, connectors, power distribution board brackets1.45–1.55 g/cm³140–170 MPa (dry)8–12 kJ/m² (dry)V-0 @ 1.5 mm
GRN-PBT-E510Flame-retardant glass-fiber-reinforced PBT (high CTI)Connectors, ESC brackets1.55–1.70 g/cm³100–130 MPa6–10 kJ/m²V-0 @ 1.5 mm
GRN-PCA-N510Halogen-free flame-retardant PC/ABSBattery housings, remote controller housings1.17–1.20 g/cm³55–65 MPa10–30 kJ/m²V-0 @ 1.5 mm
GRN-PC-N510Halogen-free flame-retardant PCBattery housings (when heat requirements are higher)1.20–1.24 g/cm³60–68 MPa20–50 kJ/m²V-0 @ 1.5 mm
GRN-PCA-H320Low-temperature high-impact PC/ABS (non-flame-retardant)Body housings, remote controllers, landing gear1.12–1.15 g/cm³48–56 MPa45–65 kJ/m² (−30 °C: 25–40 kJ/m²)HB @ 1.5 mm
GRN-PCA-W310Weather-resistant PC/ABS (non-flame-retardant)Outdoor appearance parts, cargo boxes1.12–1.16 g/cm³50–58 MPa35–55 kJ/m²HB @ 1.5 mm
GRN-PCAS-W310 / GRN-ASA-W110Weather-resistant PC/ASA / weather-resistant ASA (non-flame-retardant)Radomes, payload bays, cargo boxes1.06–1.17 g/cm³40–60 MPa8–50 kJ/m²HB @ 1.5 mm
GRN-PC-L110Transparent PC (non-flame-retardant)Lens protectors, indicator covers, transparent radomes1.19–1.21 g/cm³60–68 MPa60–80 kJ/m²HB @ 1.5 mm
Aluminum alloy (reference)——About 2.7 g/cm³———
  • Typical values. Refer to the actual TDS. Low-temperature impact is provided at the temperature you specify. Fatigue and vibration data are to be verified by GREENPOLYMER and can be tested per project.
  • For full properties, see Products. For how to choose, see the selection guide.

Why GREENPOLYMER

  • Custom compounding

    GREENPOLYMER does carbon fiber and glass fiber reinforcing, toughening, flame-retardant and weather-resistant compounding. Formulations can be adjusted to the different requirements of arms, battery compartments and radomes. Materials marked "Available as a project-based development" in the table can be developed with GREENPOLYMER engineers.

  • Prototype to production

    GREENPOLYMER makes both pellets and 3D printing filament. During development, arms and brackets are printed in carbon fiber PA filament; for mass production, they switch to injection molding with the equivalent pellets.

  • Technical support

    Material selection assessment and design advice on wall thickness and ribs; mold flow analysis can be done together with your tooling team.

  • Halogen-free flame retardancy

    GREENPOLYMER's flame-retardant technology focuses on halogen-free and fluorine-free solutions. Silicone-based flame-retardant grades do not use PTFE anti-drip agents.

  • Color matching

    The Shenzhen Color Matching Center works to RAL and Pantone numbers and customer color plaques. UV-resistant compounding can be added for appearance parts.

  • Recycled grades

    Each grade can be customized with recycled content (suffix -R). The recycled share is set per project, with traceability documents. Certificate to be uploaded.

  • Fast sampling

    Free samples of 1–5 kg are available for standard grades, usually shipped in 3–7 working days. Custom formulation samples usually take 1–3 weeks.

  • Sites

    The company headquarters and main plant are in Jiangxi, which is also home to a 3D printing filament industry cluster. GREENPOLYMER also has the Hangzhou Production Base, the Shenzhen Color Matching Center and the Dongguan Development Center. 6,000+ t capacity; 29,000+ m² total plant area.

  • Patents

    8 invention patents.

  • In-house testing

    Test equipment covers melt flow rate, Izod and Charpy impact, horizontal and vertical burning (UL 94 method), heat deflection temperature and Vicat, constant temperature and humidity, UV and xenon-arc weathering, XRF, TGA, DSC, glow-wire, needle flame, comparative tracking index (CTI) and salt spray. In-house tests are for development and quality control and do not replace third-party test reports or UL certification.

  • Customers and partners

    DJI.

3D printing in drone development

UseExampleRecommended filament
Structural prototypesAssembly and flight validation of arms, center frames and motor mountsGRN3D-PA6-C20 (PA6 with 20 % carbon fiber; carbon fiber content to be verified by GREENPOLYMER); GRN3D-PA12-C10 (lower moisture absorption); GRN3D-PA6-G25
Payload bracketsQuick-release mounts for cameras, LiDAR, spray nozzles and lightsGRN3D-PA6-C20; GRN3D-PETG-C01
Antenna and sensor mountsVideo transmission antenna mounts, GNSS brackets (no carbon fiber)GRN3D-ASA-S01 (outdoor); GRN3D-PETG-S01; GRN3D-PC-E01
Flexible partsLanding gear feet, damping pads, cable jacketsGRN3D-TPU-F95; GRN3D-TPU-F85
Appearance samplesAppearance reviews of body and remote controller housingsGRN3D-PLA-M01 (Matte); GRN3D-PCA-E01 (PC/ABS)
  • The properties of printed parts depend on print orientation, layer thickness and infill. Run vibration and drop tests on arms and motor mounts as actually printed.
  • Carbon-fiber-reinforced filament may conduct electricity and may affect wireless signals.

For filament details, see the filament overview, Engineering series, Everyday Functional series and Flexible series. To prototype in filament and then injection-mold the same material family, see From compounding to filament. For more 3D printing applications, see the 3D printing industry page.

Industry FAQ

Q1. Carbon-fiber PA or carbon tube for drone arms?

Both are common. Carbon tubes with plastic joints suit long arms and heavy-lift drones. Molded CF-PA suits small and medium arms and folding arms. It forms complex shapes in one step with consistent quality. CF-PA has a lower modulus than carbon tube and absorbs moisture, so validate under real vibration and drop conditions.

Q2. Can antenna covers use carbon-fiber material?

Not recommended. Carbon fiber conducts electricity and blocks radio signals. Use non-conductive materials such as PC, ASA or PC/ASA, and avoid metallic pigments. Measure dielectric constant and loss when needed.

Q3. What flame rating do drone battery housings need?

Flame-retardant materials are generally used around lithium batteries. The rating is set by the OEM's material specification and must be assessed at the actual wall thickness. GB 42590-2023 requires no fire or explosion in the drop and battery-pack tests, but sets no flammability rating for housing materials. Our halogen-free FR PC/ABS and PC grades target V-0 @ 1.5 mm; refer to the test reports.

Q4. Will housings become brittle in winter flights?

Standard ABS and some PC/ABS lose toughness at low temperatures. For winter or high-altitude use, choose a low-temperature high-impact grade and test impact at −20 °C or −30 °C. GRN-PCA-H320 has −30 °C impact data (typical values).

Customers and partners

  • DJI

Request a quote / sample

Please tell us:

  • Drone type (consumer, industrial, crop protection, logistics) and part name
  • Temperature range and outdoor exposure time
  • Flammability, weathering and signal transmission requirements
  • Current material
  • Prototype or production; estimated annual volume
  • TDS / SDS: Chinese and English versions are available by email.
  • For samples and the development process, see the FAQ.

Contact us

Tell us about the part, material requirements, equipment and expected volume. We will recommend suitable grades and the validation data you need.