Soyuz “Globus” Mechanical Navigation Computer

Remember: “Globe Theory”

Also, one of the Big Questions RE supposed space flight, rocket launches, etc. is the absolutely total absence of any and all rocket engine noise and roar that surely should have been overwhelmingly loud (and therefore at least somewhat audible in all recordings, completely contrary to all available evidence) given the propinquity of the astronauts and their microphones to the blasting engines.  Had NASA perfected noise cancelation all those decades ago and just never told anybody?

Clearly, massive, expensive, intricate work was put in and machinery exists consistent with such huge undertaking.  If under cover of deception(s), what were the actual goals?  Look at this masterpiece.  Reminds of the Sperry gyroscope and S-band microwave radio(s) investigated (I believe) by the same youtuber.




The Soyuz “Globus” mechanical navigation computer, also known as “Globus” or “Globus IMU” (Inertial Measurement Unit), is a sophisticated mechanical device used in the Soyuz spacecraft for navigation, guidance, and control during space missions. Developed by the Soviet Union, the “Globus” played a crucial role in ensuring the accurate orientation and maneuvering of the spacecraft in space.

Key features and functions of the Soyuz “Globus” include:

1. **Inertial Measurement**: The “Globus” is an inertial navigation system that uses gyroscopes and accelerometers to measure the spacecraft’s orientation, velocity, and acceleration relative to its initial reference frame. This information is essential for maintaining the spacecraft’s desired trajectory and attitude during different phases of the mission.

2. **Mechanical Design**: Unlike modern digital navigation systems, the “Globus” is a mechanical device composed of rotating gyroscopes and pendulous accelerometers housed within a sealed chamber. The mechanical components are finely crafted and balanced to provide accurate measurements even in the microgravity environment of space.

3. **Redundancy and Reliability**: The “Globus” is designed to operate autonomously and independently of external inputs, providing redundancy and reliability in navigation and guidance tasks. It is capable of maintaining accurate navigation solutions even in the event of system failures or communication disruptions.

4. **Integration with Flight Control System**: The output from the “Globus” is integrated with the spacecraft’s flight control system, allowing the onboard computers to continuously update the spacecraft’s attitude and trajectory based on the navigation data provided by the “Globus.” This integration ensures precise control and maneuvering capability during critical mission phases such as orbit insertion, rendezvous, and docking.

5. **Historical Significance**: The Soyuz “Globus” has been used in various iterations of the Soyuz spacecraft since the 1960s and has played a vital role in numerous manned space missions, including orbital flights, space station dockings, and crew transfers. Its reliability and performance have contributed to the success of the Soviet and Russian space programs over several decades.

Overall, the Soyuz “Globus” mechanical navigation computer represents a remarkable achievement in space technology and continues to serve as a cornerstone of navigation and guidance systems in the Soyuz spacecraft, ensuring the safe and precise execution of manned space missions.

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