by lexperience » Wed Jun 12, 2019 7:38 am
1. Nuber of crew, people --- up to 3
2. Starting mass, kg --- 7150, 7190
3. Launch vehicle --- "Soyuz", "Soyuz-2"
4. Parameters of the satellite orbit:
- inclination, degrees --- 51,6
- elevation of the orbit, km --- 202 / 242
- maximum permissible circular height working orbit, km
-- when docking the ship with the station --- 425
-- during the descent of the ship --- 460
5. Rated fueling of KDU fuel, kg --- 840
6. Estimated payload mass, kg
delivered to the station with a crew of 3 people --- up to 100
delivered to the station with a crew of 2 people --- up to 200
with a crew of 3 people returned to Earth --- 50
when returning to Earth with a crew of 2 people --- 120
7. Maximum flight duration, days --- 210
including autonomous, day (of them without BW - up to 18 turns) --- 4, 2
8. Maximum deviation of the landing point SA (circle radius), km --- 20
with the accuracy of reduction at 10 km altitude (radius of the circle), km --- 15
9. Geometric characteristics:
ship length according to hull, mm --- 6980
maximum diameter (across the frame of the joint with PH), mm --- 2720
diameter of residential compartments, mm --- 2200
span of solar cells, mm --- 10700
volume of residential compartments in gas, m3 --- 10
diameter of the landing hatch BO, mm --- 660
manhole diameter SA, mm --- 600
diameter of the passage hatch between the ship and the station, mm --- 800
diameter of visual windows, mm --- 228