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"11. TECHNICAL CHARACTERISTICS OF THE REUSABLE SPACE TRANSPORT SYSTEM AND ITS COMPONENTS

11.1. Orbital plane

11.1.1. Overall dimensions, m:
length - 41.4
height including vertical tail (without landing gear) - 14.5
wingspan - 26
cargo compartment diameter - 5
cargo compartment length - 20

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"

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