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The receiver has a probe, which is a rigid, protruding or pivoted retractable arm placed on the aircraft's nose or fuselage to make the connection. Most modern versions of the probe are usually designed to be retractable, and are retracted when not in use, particularly on high-speed aircraft. [citation needed]
The aircraft was accepted into service in 1983. Su-24M has a 0.76 m (30 in) longer fuselage section forward of the cockpit, adding a retractable refueling probe, and a reshaped, shorter radome for the attack radar. It can be identified by the single nose probe in place of the three-part probe of earlier aircraft.
This baseline version includes a fully retractable refueling probe and an interconnecting drive system for power redundancy. [9] In addition, the Bell-Boeing team included eight possible variants, or "excursion designs", including a sea-based variant.
RF-84F with a retractable probe for hookup with carrier GRB-36Ds and tailplanes with marked anhedral, 25 redesignated from RF-84F. [6] XF-84H Two F-84Fs were converted into experimental aircraft. Each was fitted with an Allison XT40-A-1 turboprop engine of 5,850 shaft horsepower (4,365 kW) driving a supersonic propeller.
As built, the Tu-22M included the provision for a retractable probe in the upper part of the nose for aerial refueling. The probe was reportedly removed as a result of the SALT negotiations, because with refueling it was considered an intercontinental range strategic bomber. [88] The probe can be reinstalled if needed. [2] [self-published ...
A Russian Air Force (VVS) Ilyushin Il-78 tanker aircraft with its two hose and drogue refuelling devices extended is followed by two Sukhoi Su-24 attack jet aircraft simulating aerial refuelling, flanked by four smaller Yakovlev Yak-130 trainer/fighter aircraft, from the celebration flypast during the Moscow Victory Day Parade of 2010.
The aircraft is fitted with retractable tricycle landing gear, with a double-wheeled nose gear and single main wheels. [100] A pair of air brakes are located on the sides of the rear fuselage; the canards also angle downward to act as air brakes and decrease landing distance. [101] It is capable of flying at a 70–80 degrees angle of attack. [102]
A retractable nose-mounted refueling probe was also fitted. Other optional equipment included a tactical air navigation system (TACAN) receiver and a drogue parachute, the latter of which could be used to assist braking during land operations.