SHAF R-102
The SHAF R-102 was the last aircraft designed by Antonius Raab Aeronautical Laboratory, in 1972. It was a scaled up Lockheed JetStar, powered by four Aerodyne TF110-AD-50, the first turbofan engine of Aerodyne Engines. With the fan at the back, TF110-AD-50 and the more powerful TF110-AD-65 (6,750 lbf instead of 5,000 lbf) were similar with the General Electric CJ805. TF110 reached 10,500 lbf of thrust during developing trails, but production engines were downgrated for maximum possible fuel economy. Fuselage of R-102 had exactly the same diameter with the JetStar, but it had a more efficient wing, allowing in to reach high subsonic speed at altitube. Prototype actually break marginally the sound barrier in dive during trails. The R-102B was longer and had also larger wing with increased fuel capacity and extra pinion tanks, enough to cross Atlantic from Athens flying at economic speed under two engines. Approximately 160 airframes build total, most in civilian hands from 1976 to 1989.
Only military users were Hellenic Kingdom and Cyprus (latter had the MP variant with Guardian radar and ISI Serapis Mk2 MIMS). The R-102MP had eight pylons, two under the fuselage (similar with F-104G) and three under each wing (of which inner were "'wet"). Fuselage pylons were the strongest, capable of suppoting AM-39 or Gabriel IIIAS missiles while rest hold various pods (gun, rocket) or TP-1/TP-2 torpedoes. RHAF R-102EW were regular visitors of Paphos Air Base, while Cypriot 446th Naval Regiment had also 8-10 R-57CS.
Note that from all those 102 design numbers about half remained on paper, because Raab numbered every design-even marginally changed from previous. Among his designs were microlites, sail planes, fighters, bombers, transport aircrafts, small private aircraft, Some designs sold to other countries as well, among these "export" designs were microlites, sailplanes and small private aircraft.