IN FLIGHT RESEARCH & TEST CENTER

CCIZ Results

Significant results of research:

  • AIRCRAFT:
    • SUPERSONIC:
      • Test and evaluation for certification and homologation of upgraded aircraft MIG 21 LANCER;
      • Test and evaluation for certification of configuration with rockets and some types of bombs for MIG 21 LANCER aircraft;
      • Test and evaluation for certification of final version of MIG 21 LANCER flight operational program;
      • Test and evaluation for certification of MIG 21 LANCER aircraft  to Air-to-Air firing with aircraft’s gun;
      • Test and evaluation for validation of MIG 21 LANCER configuration with MAGIC 2 rocket;
    • SUBSONIC:
      • Test and evaluation for homologation of IAR 93 in all versions;
      • Test and evaluation for certification/homologation of IAR 99 aircraft;
      • Test and evaluation for certification/homologation of IAR 99 ŞOIM aircraft;
      • Test and evaluation for certification of IAR 99 ŞOIM equipped with a ventral fins system;
      • Flight test of advanced training system for IAR 99 ŞOIM aircraft;
      • Flight test for certification of IAR 99 ŞOIM aircraft to Air-to-Air firing with aircraft’s gun;
      • Flight test for IAR 99 ŞOIM aircraft certification for unguided reactive projectile firing in MAN mode;
      • Integrating IAR 99 Flight Simulator into ATN network through ACTS ground station;
      • IAR 99 ŞOIM virtual designed prototype for aeronautic studies;
      • Integrated system for visualizing IAR 99 ŞOIM trajectory by using SAIMS system’s recordings;
      • Calibrating ROMBAC-1-11 aircraft’s system of speed measurement;
      • Homologation of IAR 827 aircraft;
      • Homologation of IAR AG 6 aircraft.
  • HELICOPTERS:
    • In flight and on ground vibration program for IAR 330 SOCAT helicopter (Integrated System for determining the vibrating level of IAR 330 SOCAT helicopter by analysing the SAIMS system recorded data);
    • In flight measurements for determining the stability derivates for IAR 316 B, IAR 330 H and IAR 330 L;
    • Test and evaluation for the certification / homologation of IAR 330 PUMA NAVAL used on F22 frigate;
    • Integrated system for the analysis of SOCAT (VRGE) flight missions;
    • Ballistic protection manufacturing solution for IAR 330 PUMA SOCAT armor system;
  • UAV:
    • Acceptance test and evaluation for SHADOW 660 UAV;
    • Test and evaluation for certification / homologation of UAV – target for aerial firing exercises.
  • ROCKETS:
    • Test and evaluation for certification and homologation of air-to-air guided missiles and air-to-ground unguided rocket launchers;
    • Test and evaluation for certification and homologation of RT 759M target rocket for RSA/RAA system firing;
    • Test validation of 5Ia23 VOLHOV rockets’ performance which uses oxidant special fuel with expired physical – chemical characteristics (over 6% water);
  • AVIATION ENGINES:
    • Test and evaluation for homologation of VIPER engine equipped with afterburner. In flight test and instrumentation of in flight test.
  • EJECTION SEATS SYSTEMS:
    • In flight and on ground test and evaluation for homologation of Romanian HV-0 ejection seat
    • Integrating pilots surviving equipment with flight equipment, DASH system, ejection seat and IAR 99 ŞOIM cockpit;
  • AVIATION EQUIPMENTS:
    • Acquisition, recording and tele-transmission system for ground and onboard equipments for adjusting and monitoring aerial bombing;
    • Onboard video pod;
    • Aircraft store separation study. Determining the release envelope;
    • Measuring system for pilot electro-physiologic signals during testing;
    • Measuring and computing system for vibration signals;
    • Overload meter;
    • Data acquisition onboard-mounting system with static memory;
    • Test and evaluation for certification / homologation of radio-navigation, communication and beaconing system for military airports;
    • Live monitoring system for operative interest  and high potential risk areas (SMTR);
    • Elaboration of software application for rapid analyze and identify of exceeding admissible threshold of PUMA-SOCAT flight parameters;
    • Integrated system for visualizing the aircraft’s trajectory on short periods of time by using SAIMS system’s recordings;
    • In flight and on ground test and evaluation for homologation of Trelleborg sealing solution. Decision making though tests for reconsidering the technical life – Modernizing hydraulic actuators (SMHR-eD);
  • AVIATION AMMUNITION
    • Validating the compatibility between the 20mm caliber projectile and the IAR 330 SOCAT helicopter’s gun;
    • Test and evaluation – NATO compatible BAEF-250M aviation bomb;
    • Test and evaluation – Small caliber practice bomb;
    • Test and evaluation MIG 21 LANCER configuration with BAEF-500 NATO standard bomb;
    • Testing aircraft countermeasure systems;
    • Test and evaluation of aviation bomb fuses;
    • Test and evaluation for aviation bombs’ homologation;
    • Test and evaluation for unguided rockets.