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One of the few, if not the only, V24 engines in current production is the Austrian-made Jenbacher J624 gas engine for electric power generation and CHP applications. The engine makes use of two-stage turbocharging, and with a bore and stroke of 190mm by 220mm, the total swept volume of the 24-cylinder engine is 149.7L.
The V-24 is a T-tailed twin engine composite construction pusher aircraft with retractable tricycle landing gear. The aircraft will be powered by either Rotax 912, or 160 hp Lycoming IO-320 engines. The aircraft has a Galaxy GRS 1200 parachute system integrated into the airframe. Turboprop engines are also under consideration. [1] [2]
Mil V-24, a Soviet helicopter prototype; Softex-Aero V-24, a Ukrainian light aircraft; Other uses. ITU-T V.24, a telecommunications standard; V24 engine
V-24 The first version, twelve prototypes and development aircraft. The first V-24 mockup resembled the Bell UH-1A Huey. Later models resembled the future Hind-A, one of which was modified in 1975 as A-10 for speed record attempts with wings removed and faired over and with inertia-type dampers on the main rotor head. The A-10 reached a speed ...
V.24 is referenced as RS-232 which also includes V.28. V.25ter see V.250; V.27ter is an ITU-T recommendation for a half-duplex modem, allowing 2400 and 4800 bit/s (PSK modulation). V.28 is an ITU-T recommendation defining the electrical characteristics for unbalanced double-current interchange circuits.
The voltage range was extended to ±25 volts, and the circuit capacitance limit was expressly stated as 2500 pF. Revision E of EIA-232 introduced a new, smaller, standard D-shell 26-pin "Alt A" connector, and made other changes to improve compatibility with CCITT standards V.24, V.28 and ISO 2110. [7] Specification document revision history:
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The Softeks V-24 Lastivka (Ластівка, Swallow) is a four-seat, twin pusher engined utility aircraft, designed and built in Ukraine in the 2010s for survey and transport work. The first prototype flew late in 2012.