Energia - Buran Space Transportation System

Diagram of the Buran control system. The heart of it was the computer system, which consisted of 8 Biser-4 multiprocessor computers (red color). In total the system had 32 processors. The image also shows in blue the quartz generator with its five redundancy channels.
 

Attachments

  • bbur197.jpg
    bbur197.jpg
    775.2 KB · Views: 154
Some rare but interesting views of two optical systems of the Buran:

Visual Navigation Measurement System (NIVS)
This system would be used for approach and docking maneuvers in orbit (together with other means).

Stellar-Solar Instrument (ZSP)
A set of star trackers designed to determine Buran's position and orientation in orbit. These data would then be used to remove the error from the three so-called Gyro-Stabilized Platforms (GSPs).
 

Attachments

  • Buran NIVS ZSP GSPs anotations.jpg
    Buran NIVS ZSP GSPs anotations.jpg
    354.1 KB · Views: 83
  • Buran Visual Navigation Measurement System NIVS.jpg
    Buran Visual Navigation Measurement System NIVS.jpg
    308.2 KB · Views: 40
  • Buran Stellar-Solar Instrument ZSP.jpg
    Buran Stellar-Solar Instrument ZSP.jpg
    147.3 KB · Views: 40
  • 20230718160045-f792b1e0-3.jpg
    20230718160045-f792b1e0-3.jpg
    233.8 KB · Views: 49
Interesting panoramic views of Buran #1, during the preparations in Baikonur for its first (and last) launch in November 1988.To highlight in the views, the 37KB module for the collection in this mission of the very valuable flight data.
 

Attachments

  • Pano0.jpg
    Pano0.jpg
    1,003.4 KB · Views: 33
  • pano1-procesada.jpg
    pano1-procesada.jpg
    442.9 KB · Views: 32
  • pano2-procesada.jpg
    pano2-procesada.jpg
    218.9 KB · Views: 39
  • Buran-detras-cabina-bodega2.jpg
    Buran-detras-cabina-bodega2.jpg
    550.2 KB · Views: 49
In 1977, a decision was made to develop radio altimeters to measure flight altitude during the descent and landing modes of the reusable Buran shuttle. Developed by UPKB Detal, the Low-Altitude Radio Altimeter A-039 «Polosa» was intended for automatic landing, and the High-Altitude Radio Altimeter A-067 «Virazh» was intended directly for measuring flight altitude in the descent and landing modes of the Buran in the altitude range from 0.5 to 25 km. The famous only flight of the Buran in November 1988 took place largely thanks to the radio altimeters developed at UPKB Detal, with the help of which the soft landing of the Buran was carried out in automatic mode.
 

Attachments

  • Polosa A-039 Buran Radio altimeter low altitudes-enhance.jpg
    Polosa A-039 Buran Radio altimeter low altitudes-enhance.jpg
    316.9 KB · Views: 33
  • Virazh A-067 Buran Radio altimeter high altitudes-enhance.jpg
    Virazh A-067 Buran Radio altimeter high altitudes-enhance.jpg
    283.1 KB · Views: 33
Deciphering the Buran

Some elements of the Buran, seen in these photos:

1 - Accelerometers
2 - RVV (Vertical Radio Altimeter) / PMV (Infrared Horizon Sensors)
3 - Window
4 - GSPs (Gyro-Stabilized Platforms)
5 - NIVS (Visual Navigation Measurement System)
6 - ZSP (Stellar-Solar Instrument)
7 - ZSP's protective cover
8 - Electronics boxes
9 - Hatch

equipos1-1.jpg
 

Attachments

  • bur#2-interior-2x-original-contrasted3.jpg
    bur#2-interior-2x-original-contrasted3.jpg
    564.6 KB · Views: 30
  • Buran-detras-cabina-bodega2-2-frame.jpg
    Buran-detras-cabina-bodega2-2-frame.jpg
    418.8 KB · Views: 25
Well, one of the test articles is on display at the Technik Museum, Speyer, Germany. I saw it there a few years ago.

2560px-OK-GLI_Technik_Museum_Speyer_2008_12.JPG
 
Yes, the truth is that they are incredible machines, with a quality of manufacturing to highlight... Those who have visited these spacecrafts in Baikonur, the so-called "explorers of the Buran", sometimes highlight that the interior of them looks "as if recently left the factory", even though they have been heavily vandalized. But they can still be rescued. Some time ago, Dmitry Rogozin, when he was the Head of Roscosmos, mentioned that it is the Russian Federation's intention to one day return these spacecrafts to Russia. The issue is complicated, because as I understand it, the Buran of Baikonur are owned by a businessman from Kazakhstan. Greetings!
 
Two important devices for the Buran's navigation system: accelerometers and the angular velocity sensor. Both devices were developed by the Pilyugin Center (JSC NPTsAP), which also developed the Buran's «Biser-4» (SH16M) computer.
 

Attachments

  • Buran Accelerometers.jpg
    Buran Accelerometers.jpg
    151.1 KB · Views: 39
  • Buran angular sensor.jpg
    Buran angular sensor.jpg
    126.9 KB · Views: 38
Unlike Columbia style OMS pod engines (now Orion’s service module engines)—Buran’s two big engines burned sintin…ultra/refined kerosene. Buran able to maneuver better without SSME’s weighing it down.

How much greater performance could it have had over a Columbia type orbiter?
 
The RD-0120 engines are a fascinating divergence from our hydrolox engines. Amazing pieces of engineering. Both ours and their hydrolox engines had positives and negatives and both former soviet and our American engineers learned from one another's designs.
 
Unlike Columbia style OMS pod engines (now Orion’s service module engines)—Buran’s two big engines burned sintin…ultra/refined kerosene. Buran able to maneuver better without SSME’s weighing it down.

How much greater performance could it have had over a Columbia type orbiter?
unsupported statement. not based on facts or engineering.
 
Ghostly image of Buran #2, in the MZK building in Baikonur.
It is said that this shuttle was 95% finished, with all its equipment installed, 37KB module, docking module, robotic arm, etc etc.... Those who have visited it say that it is impossible to transmit the enormous size of this “thing”!!!
After the program was cancelled, the Russians removed all the electronics to end up in these last years being vandalized by some furtive visitors. But it can still be rescued! Her interior looks like fresh from the factory. Hopefully it will one day end up safe in a museum.

vlcsnap-2024-05-03-19h21m59s264.jpg
 
Rare views of the so-called «ZSP» (Stellar-Solar Instrument), a set of star trackers that measured the line-of-sight vector to at least two stars. Using this information, the on-board computers calculated the orientation between these stars and the orbiter to determine the vehicle's attitude. (Bart Hendrickx)

vlcsnap-2024-05-11-18h48m49s981-anotations.jpg

vlcsnap-2024-05-11-18h48m49s981-anotations2.jpg

BURAN ZSP.jpg
 

Similar threads

Please donate to support the forum.

Back
Top Bottom