11.1.2. Mass characteristics, t:
at the moment of launch of the MTKS on the AES with an inclination to the equatorial plane i=51.6° - 171
on an AES with an apogee of 200 km and a perigee of 80 km (i = 51.6°) - 154
on the satellite with Ncr=200 km (i = 51.6°) - 152
structure - 94.5
during normal landing - 115
during an emergency landing - 164
fuel for recovery from an emergency during the first 40 seconds of flight - 6.78
fuel for orbital maneuvering and jet control (working reserve) - 23.76
11.1.3. Number and types of engines:
second stage - 4 oxygen-hydrogen liquid fuel engines
orbital maneuvering - 2 liquid fuel engines
reactive control - 40 liquid reaction control engines, 10 vernier engines"