Air Systems Research Center
The Air Systems Research Center conducts research, test and evaluation on aircraft, related components and missiles.
Aircraft Research Division
Research on system integration of aircraft and component technology for aircraft, aircraft-related equipment and missiles.
Engine Research Division
Research on system integration of engine and component technology for aircraft and missiles.
Missile Research Division
Research on system integration of missiles and component technology for missiles.
Environmental test and combustion test of rocket motors.
Service for firing test of missiles.
Integrated Fire Control for Fighters
Integrated Fire Control for Fighters is a key technology in future network centric warfare environment in air-to-air combat. Resource sharing of onboard active/passive sensors and weapons among fighter formation via local secured datalink will realize an air superiority to stealth and/or outnumbering enemy aircraft.
Weapons Bay System for Stealth Fighters
Weapons Bay System is one of the essential subsystems for stealth fighters. Housing stores within weapons bay have twofold benefit: reduced extra drag and smaller radar signature (by non-existence of any pylons and any external stores) . The system needs to work properly and launch weapons in a very short reaction time at high speed and high maneuver flight condition.
Intake Duct for Stealth Fighters
A Serpentine Intake Duct is considered as an effective measure to reduce radar reflection from an engine. Design technology with CFD analysis and boundary layer separation controls is investigated to solve air flow degradation caused by the serpentine. Thus both stealth and favorable aerodynamic characteristics are incorporated in the intake duct.
Research on lightweight airframe structure
In order to suppress weight increase, this research will investigate lightweight airframes using efficient and accurate structural analysis techniques, an integrated bonded structure with a greatly reduced number of fasteners and a high-performance heat-shield.
Electric Actuation Technology
Electric actuation system for flight control, landing gear retraction, steering and braking will replace present hydraulic system.
Airborne Sensor System for Ballistic Missile Warning
Airborne sensor system of IR sensor mounted on UAV is integrated for ballistic missile warning.
High-Power Slim Engine Technology
Thrust Vectoring Control Technology
3D thrust vectoring nozzle with all-around 20 degrees vectoring capability enables future fighter to achieve high maneuverability.
Technology of Direct Filament Winding Multi-segment Propellant Rocket Motor
Direct Filament Winding (DFW) Multi-segment Propellant Rocket Motor is investigated for the purpose of improving flight performance of guided missile and reducing production cost. Fundamental change of manufacturing method of rocket motor enables design flexibility of thrust pattern and large improvement in mass ratio.
Missile Guidance Technology in High Altitude & Speed Target
Missile guidance technology for high speed target in high altitude realizes Surface to Air Missile System to cope with low orbital theater (or tactical) ballistic missile and hypersonic velocity cruise missile in the future. Elements of this technology include Side Thruster against long periods of high pressure combustion, Thrust Vector Control (TVC) by jet tubs and high response Missile Guidance Algorithms.
Predictive Optimal Guidance and Control Technology
This technology reinforces missiles to cope with low RCS and high maneuverability target by application of model predictive control or optimal method to missile guidance.
Millimeter Wave Fire Control Radar Technology
Technology for millimeter wave fire control radar enables detection and tracking of seaborne, ground and aerial threats.
Future Fire Control Radar Technology
Technologies for future fire control radar enable detection and tracking of stealth Fighter / Bomber, high speed ASM and low altitude CM that are difficult to detect and track by conventional technologies.
Test Records the Next-Generation Cargo Aircraft (XC-2)
The full-scale static and fatigue strength tests of the XC-2, developed mainly as a replacement for the C-1 cargo aircraft of the Japan Air Self-Defense Force, were completed.【Test Period：FY2006-2016 】
Test Records : Advanced Technology Demonstrator(X-2)
This is an experimental aircraft designed for evaluating the maturity and integration of advanced airframe and engine technologies for future fighters. The full-scale static strength test and of the engine test (Altitude Test) of the X-2, were completed.【Test Period：FY2012-2015 】
Test Records: Next-Generation Maritime Patrol Aircraft (XP-1)
The test program of the XP-1, developed as a replacement for the P-3C maritime patrol aircraft of the Japan Maritime Self-Defense Force, was completed. [Test Period: FY2006-2012]