METHOD OF TETHERING BALLOON CIRCULAR VIEW RADAR CONSTRUCTING
INSTALLATION OF RADIOTRANSPARENT FAIRING ON AIRCRAFT BODY
MANUFACTURING METHOD OF WEDGE-SHAPED RADAR-TRANSPARENT FRONT FAIRING OF SUPERSONIC AIRCRAFT BODY
METHOD OF DISCHARGING POWER FROM GYRO OF SPACECRAFT WITH CREATING THE MAGNETIC MOMENT
NAVIGATIONAL RADIOOPTICAL ANGLE REFLECTOR OF DIRECTIONAL ACTION WITH LIGHT-REFLECTING FACES
NODES FOR EXTERNAL ANCHORING CONTAINERS OF ONBOARD SENSORS TO AIRCRAFT FUSELAGE
EXPANDABLE DESIGN OF THE DIFFRACTION OPTICAL SYSTEM WITH LARGE APERTURE
PRODUCTION OF SUPERSONIC AIRCRAFT FUSELAGE FRONT WEDGE-SHAPE RADAR DOME