Документ взят из кэша поисковой машины. Адрес
оригинального документа
: http://www.buran.ru/htm/mol-300.htm
Дата изменения: Unknown Дата индексирования: Tue Oct 2 00:32:16 2012 Кодировка: Поисковые слова: п п р п п р п п р п |
Molniya Triplant Aircraft |
Molniya-300
Unlike the MOLNIYA-100 triplane roughly similar to it in dimensions the MOLNIYA-300 though is supplied with no piston, but turbojet engines. This is a six-seat business aircraft the cabin of which has all necessary conditions for rest or work. The location of the engines in the rear fuselage reduces noise and vibrations that makes multihour flights tireless. Like the MOLNIYA- 100 this jet aircraft can use airdromes with the artificial coating, as well as the ground ones. |
Molniya-300 aircraft Main Characteristics | |
Take of engine power, hp | - 2x1220 |
Maximum payload, kg | - 1350 |
Take-off mass, kg | - 6800 |
Operational range, km: | |
|
- 2900 |
|
- 5100 |
Speed, km/h: | |
|
- 930 |
|
- 800 |
|
- 160 |
|
- 195 |
Maximum fuel reserve, kg | - 2100 |
Take-off run, m | - 630 |
Landing run, m | - 460 |
Go to: | |||
Introduction |
Spiral Project |
Bor Experimental Space Vehicles |
Buran Orbiter |
Multipurpose Aerospace System (MAKS) |
Supersonic Rockets-Targets |
Company Details |
More Details in Russian |
Web-master: ©Vadim Lukashevich 1998-2005
E-mail: buran@buran.ru