ARC-1982-AC82-0402-5 | WIKIARCHIVES.SPACE

cutaway Rockwell International Space Shuttle Main Engines: Powerhead (Left side - fuel preburner, fuel trubopump - Center - Main Combustion Chamber, nozzle forward manifold - Right side - oxidizer preburner, oxidizer turbopump, preburner boost pump)

Figure 1-3.- The Space Shuttle orbiter

Figure 3-1. Orbiter structures

Figure 3-2. Dimensions of the Orbiter vehicle

Figure 3-20. Mechanical subsystems

Figure 3-21. Crew cabin ingress/egress

Figure 3-3. Forward fuselage (crew module and structure)

Figure 3-4. Crew module layout

Figure 3-5/3-6. Flight-deck crew cabin arrangement - Aft flight-deck configuration

Figure 3-7. Mid-deck crew cabin arrangement

Figure 5-1. Orbiter crew station

Figure 5-11. Galley configuration (concept).

Figure 5-12. Rigid sleep station provisions

Figure 5-13. Personal hygiene equipment on orbit locations (with galley).

Figure 5-2. Sleeping bag use locations

Figure 5-3. Operationl seats installed

Figure 5-4. Restraints (typical)

Figure 5-6. Postlanding egress routes with ejection seats

Figure 7-3. - Change in computer page lead connections to improve solder wicking

MSFC-75-SA-4105-2C

Space Shuttle orbiter

ARC-1982-AC82-0402-5

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Taken in: Other

Author: NASA

Description: cutaway Rockwell International Space Shuttle Main Engines: Powerhead (Left side - fuel preburner, fuel trubopump - Center - Main Combustion Chamber, nozzle forward manifold - Right side - oxidizer preburner, oxidizer turbopump, preburner boost pump)

Created on: Friday 4 June 1982

Albums: US SPACE PROGRAM / SPACE SHUTTLE / DIAGRAMS

Source link: https://images.nasa.gov/details-ARC-1982-AC82-0402-5

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License: Public Domain

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