• AFRL Demonstrates Near-Instantaneous Low-Spool Power Extraction

    Engineers from AFRL and industry partner Pratt & Whitney demonstrated a near-instantaneous low-spool power extraction capability as part of the Versatile Affordable Advanced Turbine Engine program. This successful effort marks the first in a series of planned demonstrations geared towards advancing

  • Pulsed-Detonation Engine Powers Manned Aircraft

    Aviation's first-ever flight test of a manned aircraft powered by a pulsed-detonation engine (PDE) was a success. An AFRL-designed PDE that produced greater than 200 lbs of thrust powered the Long EZ test aircraft, which achieved a speed of 120+ mph and an altitude of 60-100 ft. AFRL propulsion

  • AFRL Sponsors Research to Improve Antennas for Micro Air Vehicles

    As part of his project called "GameChanger," Dr. Richard James (an AFRL-funded professor from the University of Minnesota) is using the concept of objective structures to create new antennas for micro air vehicles (MAV) used for military purposes. MAVs are a type of remotely controlled unmanned air

  • US/UK Collaboration Produces New Military Laser Safety Code

    AFRL's High-Energy Laser (HEL) team successfully completed a 3-year effort to develop a new international agreement expanding an existing collaboration between the US and the United Kingdom (UK). The new project arrangement, entitled "Probabilistic Risk Assessment (PRA) Methods for Military Laser

  • Engineers Demonstrate Pulsed Thermography Inspection for GLOBUS II

    Engineers with the Air Force Research Laboratory's Materials and Manufacturing Directorate (AFRL/RX) performed an onsite pulsed thermography inspection of the GLOBUS II radar cover, demonstrating the capability of this new inspection technique. GLOBUS II is a radar system located at Vardo, Norway,

  • New Device Provides Active Thermal Control of Spacecraft Surfaces

    The Air Force Research Laboratory's Materials and Manufacturing Directorate (AFRL/RX) successfully integrated technologies to develop a thermal emission management system suitable for use in space. The management system requires very little power (The space environment is a harsh one that includes