Document ID: chunk:federal_register_of_legislation:F2024L01100:clause:1_35:p1
Version: federal_register_of_legislation:F2024L01100
Segment Type: clause
Provision Reference: sch 1 cl 35 (pt 1/2)
Character Range: 34395–38217

35        ML11.a                               1.    Radar and laser radar systems, direction finding equipment for determining bearings to specific electromagnetic sources or terrain characteristics, specially designed for military use and specially designed for Rockets, missiles or UAVs, capable of delivering a payload of at least 500 kg and having a range of at least 300 km.
                                               1.    Guidance and navigation equipment, as follows:
                                               1.         Specially designed for MANPADS or cluster munitions.
                                               1.        meeting or exceeding specified performance at linear acceleration levels exceeding 25 g if for rockets, missiles, or UAVs, capable of a range of at least 300 km.
                                               2.         in development and funded by US Department of Defense and for rockets, missiles, or UAVs, capable of a range of at least 300 km.
                                               1.    Electronic equipment for re-entry vehicles.
                                               2.    GNSS receiving equipment, specially designed for military use, and designed or modified for airborne applications and capable of providing navigation information at speeds in excess of 600 m/s.
                                               3.    Global Positioning System (GPS) receiving equipment specially designed or modified for airborne applications and specially designed for encryption or decryption (e.g., Y-Code, M-Code) of GPS precise positioning service (PPS) signals.
                                               4.    GNSS receiving equipment designed or modified for airborne applications and specially designed for use with an antenna that:
                                               1.         Employ four or more elements, electronically steer angular beams, independently steer angular nulls, create angular nulls with a null depth greater than 20 dB, and achieve a beam switching speed faster than 50 milliseconds;
                                               1.        Form adaptive null attenuation greater than 35 dB with convergence time less than one second;
                                               2.         Detect signals across multiple RF bands with matched left hand and right hand spiral antenna elements for determination of signal polarisation; or
                                               3.        Determine signal angle of arrival less than two degrees (e.g., interferometer antenna).
                                               1.    GNSS receiving equipment specially designed for use with rockets, missiles or uncrewed air vehicle systems capable of a range of at least 300 km and capable of delivering a payload of at least 500 kg.
                                               2.    Mobile relative gravimeters specially designed or modified for military airborne or marine use, having a time to steady-state registration of two minutes or less and having automatic motion compensation with an in-service accuracy of less (better) than 0.4 mGal.
                                               3.    Mobile gravity gradiometers designed or modified for military airborne or marine use having an accuracy of less (better) than 10 Eotvos squared per radian per second for any component of the gravity gradient tensor, and having a spatial gravity wavelength resolution of 50 m or less.
                                               4.    Inertial measurement units incorporating the following:
                                               1.         Accelerometers having a bias repeatability of less (better) than 10 µg and a scale factor repeatability of less (better) than 10 parts per million, or capable