Russia's Successful Angara-A5 Rocket Launch: A Milestone in Space Exploration

What was the duration of the engine operation during the third stage?

The engine of the third stage operated for 700 seconds.

Did the rocket achieve stable stabilization during flight?

Yes, stabilization of the rocket and parameters were in the normal range during flight.

Were there any issues with the detachment of side blocks?

No, all systems of the rocket functioned normally with successful detachment of side blocks.

How long did it take to achieve stable rocket stabilization and construction parameters?

Stable rocket stabilization and construction parameters were achieved at 510-520 seconds.

Was there any abnormal combustion pressure during the launch?

No, normal engine operation and combustion pressure were maintained at 530-540 seconds.

Did the rocket experience any malfunctions during the launch?

No, all rocket systems functioned normally throughout the launch.

How long did the rocket maintain stable propulsion and control systems?

Stable propulsion and control systems were maintained throughout the launch.

Was there any deviation from the planned flight trajectory?

No, controlled flight progression was according to the program with normal parameters.

Were there any anomalies in the engine performance?

No, engine performance was stable and confirmed throughout the flight.

Did the rocket encounter any issues with the engine shutdown and separation events?

No, stable operation of all rocket systems was maintained until engine shutdown and separation events.