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 п п п п п
Molniya-300

Molniya-300

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

Molniya-300 aircraft Main Characteristics
Take of engine power, hp - 2x1220
Maximum payload, kg - 1350
Take-off mass, kg - 6800
Operational range, km:

with maximum payload

- 2900

with maximum fuel load

- 5100
Speed, km/h:

Maximum

- 930

Cruising at alt. 3000m

- 800

Landing

- 160

Take-off

- 195
Maximum fuel reserve, kg - 2100
Take-off run, m - 630
Landing run, m - 460

 

Go to:
Introduction
Introduction
Spiral Project
Spiral Project
Bor Experimental
Bor Experimental Space Vehicles
Buran Orbiter
Buran Orbiter
Multipurpose
Multipurpose Aerospace System (MAKS)
Supersonic Rocket-Targets
Supersonic Rockets-Targets
Company Details
Company Details
Moscow Details
More Details in Russian

 

Web-master: ©Vadim Lukashevich 1998-2005
E-mail: buran@buran.ru