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Puma™ AE RQ-20B

Puma™ AE RQ-20B

Product catalog summary
Specifications and Key Features
  • Flight Endurance: Over 3 hours with an LE battery.
  • Battery Options: Smart Battery options available for various missions.
  • Payload: Gimbaled EO & IR payload with increased capacity through optional under-wing Transit Bay.
  • Propulsion System: Powerful and efficient.
  • Navigation System: Precision navigation with secondary GPS for enhanced accuracy.
  • Durability: Reinforced fuselage for improved durability.
  • Power Adapter: Plug and play secondary power adapter.
Payload Details
  • Gimbaled payload with 360-degree continuous pan and +10 to -90 degrees tilt.
  • Stabilized EO, IR camera, and IR Illuminator in a modular payload.
Performance Specifications
  • Range: 20 km.
  • Endurance: 3+ hours with an LE battery.
  • Speed: 47-83 km/h (25 to 45 knots).
  • Operating Altitude: 500 ft (152 m) AGL (typical).
  • Wingspan: 9.2 ft (2.8 m).
  • Length: 4.6 ft (1.4 m).
  • Weight: 14 lbs (6.3 kg).
Ground Control System (GCS)
  • Common GCS with Raven® and Wasp® AE.
Launch and Recovery
  • Launch Method: Hand-launched, with optional rail launch.
  • Recovery Method: Autonomous or manual deep-stall landing.
General Description

The Puma AE is a fully waterproof, small unmanned aircraft system (UAS) designed for both land and maritime operations. It can land on water or land, providing operational flexibility. The enhanced precision navigation system with secondary GPS ensures greater positional accuracy and reliability. AeroVironment’s common ground control system allows for manual control or GPS-based autonomous navigation.

Additional Information

All specifications are subject to change. This document contains general capabilities information and does not include controlled technical data as defined by ITAR or EAR regulations.

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Catalog excerpts

Puma™ AE RQ-20B-1

Puma AE (All Environment) is a fully waterproof, small, unmanned aircraft system (UAS) designed for land and maritime operations. Capable of landing in water or on land, the Puma AE empowers the operator with an operational flexibility never before available in the small UAS class. The enhanced precision navigation system with secondary GPS provides greater positional accuracy and reliability of the Puma AE. AeroVironment's common ground control system allows the operator to control the aircraft manually or program it for GPS-based autonomous navigation. SPECIFICATIONS KEY FEATURES PAYLOADS Gimbaled payload, 360 degree continuous pan, +10 to -90 degrees tilt, stabilized EO, IR camera, and IR Illuminator all in one modular payload. RANGE 20 km ENDURANCE 3+ hours with an LE battery GCS Common GCS with Raven® and Wasp® AE LAUNCH METHOD Hand-launched, rail launch (optional) RECOVERY METHOD Autonomous or manual deep-stall landing • 3+ Hour flight endurance with an LE battery • Smart Battery options to support diverse missions • Gimbaled EO & IR payload • Increased payload capacity with optional under wing Transit Bay • Powerful and efficient propulsion system • Precision navigation system with secondary GPS • Plug and play secondary power adapter • Reinforced fuselage for Improved durability AeroVironment Corporate Headquarters - Monrovia, CA 91016 USA — ph: 626.357.9983 - www.avinc.com © 2017 All product names copyright or trademark protected. All specifications are subject to change. This data sheet consists of AeroVironment., Inc. general capabilities information that does not contain controlled technical data as defined within the International Traffic in Arms Regulations (ITAR) Part 120.10 or Export Administration Regulations (EAR) Part 734.7-11. PROCEED WITH CERTAINTY

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