the future of russia’s piloted space program bart hendrickx
TRANSCRIPT
THE FUTURE OF RUSSIA’S PILOTED SPACE PROGRAM
Bart Hendrickx
Priorities in longterm space strategy (until 2030)
• Development of cosmodromes/launch vehicles and satellites for practical applications
• Space sciences• Human spaceflight
Main objectives of piloted programme 2013-2020
• ISS operations, including addition of new Russian modules (MLM, specialized modules, free-flying modules)
• Decision on continued use of Russian segment beyond 2020
• First test flights of new-generation vehicle (PTK NP)
Main objectives of piloted programme 2020-2030
• Use of new-generation vehicle and “specialized and autonomous free-flying modules” for practical applications and scientific purposes
• Development of “robotic means” to study the Moon and ensure manned flights to the Moon (including modified versions of a transport ship for flights to the Moon, a lunar landing complex and an interorbital space tug)
Main objectives of piloted programme after 2030
• Flights to cislunar space and to the Moon• Establishment of a permanent lunar base• In-orbit servicing of large space objects and
interorbital space tugs• Preparations for piloted flights to Mars “in an
international framework”
Node module (2017)
Scientific Power Module (2018)
OKA-T free-flyer (2018)
Soyuz-MS (2016)
- Improved solar panels- More docking/deorbit redundancy- GPS/Glonass sensors- Kurs-NA rendezvous system- Micrometeorite shielding
PTK NP versions
Исследовательские полёты
Возвращение на Землю
Снабжение станции
Доставка экипажа станции
Полеты к Луне
Обслуживание спутников
НАЗНАЧЕНИЕ:Транспортно-техническое обслуживание орбитальных пилотируемых станций, космических комплексов и других
объектов орбитальной группировки
Грузовозвращающий корабль
Lunar vehicle modifications
- beefed-up heatshield- improved life support systems- improved communications systems- more fuel- 4 instead of 6 crew members
СХЕМА ПРИЗЕМЛЕНИЯ ВА
Выход тормозного парашюта (H=3,2 км)
Точностьприведения <2,0 км
Точностьприземления <2,5 км
Ввод основных парашютов H=1,5 км
