Crydon Defense Systems Inc. · St. Petersburg, FL UEI ER13XF6JSQ64 · CAGE 15L43 · U.S.-owned · No FOCI
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Capability

Payload integration

Mechanical, electrical and software integration patterns that reduce interface and integration risk.

Discuss this capability

Most integration risk lives at the interfaces. Our payload integration kit captures reusable mechanical, electrical and software patterns so sensors and mission payloads reach the aircraft quickly — and work the first time at the test event.

Payload classes

  • EO/IR and imaging sensors
  • Radar, SAR and GMTI
  • SIGINT and electronic warfare
  • Communications relay
  • Customer-owned and custom payloads

Heritage in this area

The S1-V300 MALE unmanned aircraft on the apron in front of a hangar Fixed-wing

S1-V300

Medium-altitude long-endurance (MALE) UAS

endurance
28+ h
external payload
300 kg
maximum speed
220 km/h
The UVH-500 unmanned helicopter with an underslung cargo pod and a sensor gimbal Rotary-wing

UVH-500

Long-range heavy-lift VTOL unmanned helicopter

maximum range
840 km
payload, fuel included
160 kg
flight time with 20 kg
7 h
Aerial view of the ApusDuo tandem-wing solar aircraft on a grass field with its ground crew Stratospheric

ApusDuo / ApusNeo HAPS

Solar high-altitude pseudo-satellite (HAPS)

ApusDuo flight altitude, 2023
16,686 m
continuous flight, ApusNeo 18
48 h
carbon-fibre airframe
43 kg
Next step

Bring us the hard integration

Tell us about the platform, the constraints and the test event. We'll come back with an approach.

Start a conversation sales@crydon.us