File:Apollo Command Module RCS fuel tank.jpg
Original file (3,620 × 5,277 pixels, file size: 2.51 MB, MIME type: image/jpeg)
Captions
Summary
[edit]DescriptionApollo Command Module RCS fuel tank.jpg |
English: Apollo Command Module RCS Fuel Tank: An engineering test unit from Bell Aerospace in 1965. It (the fuel tank) provided Monomethylhydrazine (MMH) fuel to the spacecraft's twelve Rocketdyne SE-8 Reaction Control System (RCS) engines used for attitude control. A similar tank was used to store the oxidizer (N204 ) which was combined and ignited upon contact with the MMH. This is a hypergolic fuel system which does not require any separate ignition system.
Titanium MMH tank, with various valve connections (diagram below). Helium pressurizing gas pushed against flexible bladders in the fuel and oxidizer tanks to force the weightless propellants out of the tanks. From the Spaceaholic post on the oxidizer tank (the compliment to this tank): "The tank incorporates an integral bladder for positive expulsion. Positive expulsion systems were necessary to provide continuous propellant flow to the engines regardless of vehicle position, environmental and dynamic forces, or zero gravity conditions where the propellant tended to float in the tank and cling to the tank wall instead of flowing naturally toward the tank outlet. Propellant is contained within the bladder. A pressurizing port is provided on the tank shell and a propellant outlet port and liquid bleed tube are incorporated in the diffuser assembly. The propellant is loaded into the bladder through the propellant outlet port. When the bladder is full, helium, supplied by another onboard Command Module tank, was applied to the pressuring port of the tank to pressurize the area between the tank shell and the outside of the bladder. The pressurizing gas caused the bladder to collapse around a diffuser tube (which runs from the propellant outlet down through the center of the tank) and the propellant was expelled through the outlet port." The metal tag reads (from photo below): TANK MMH POSITIVE EXPULSION Manufactured 6-2-65 Contract NAS9-150 (indicates Apollo CSM) NAA (North American Aviation) Control Number: ME282-0007-0001 Serial Number 8 Max Working Pressure: 360 PSIG Proof Pressure: 480 PSIG Burst Pressure: 540 PSIG An artifact from the Future Ventures’ 🚀 Space Collection. |
Date | |
Source | https://www.flickr.com/photos/jurvetson/51851920746/ |
Author | Steve Jurvetson |
Licensing
[edit]- You are free:
- to share – to copy, distribute and transmit the work
- to remix – to adapt the work
- Under the following conditions:
- attribution – You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use.
This image was originally posted to Flickr by jurvetson at https://flickr.com/photos/44124348109@N01/51851920746. It was reviewed on 31 January 2022 by FlickreviewR 2 and was confirmed to be licensed under the terms of the cc-by-2.0. |
31 January 2022
File history
Click on a date/time to view the file as it appeared at that time.
Date/Time | Thumbnail | Dimensions | User | Comment | |
---|---|---|---|---|---|
current | 05:13, 31 January 2022 | 3,620 × 5,277 (2.51 MB) | Sv1xv (talk | contribs) | Uploaded a work by Steve Jurvetson from https://www.flickr.com/photos/jurvetson/51851920746/ with UploadWizard |
You cannot overwrite this file.
File usage on Commons
The following page uses this file:
File usage on other wikis
The following other wikis use this file:
- Usage on www.wikidata.org
Metadata
This file contains additional information such as Exif metadata which may have been added by the digital camera, scanner, or software program used to create or digitize it. If the file has been modified from its original state, some details such as the timestamp may not fully reflect those of the original file. The timestamp is only as accurate as the clock in the camera, and it may be completely wrong.
Camera manufacturer | SONY |
---|---|
Camera model | DSC-RX100M3 |
Exposure time | 1/60 sec (0.016666666666667) |
F-number | f/2.8 |
ISO speed rating | 125 |
Date and time of data generation | 14:17, 24 February 2021 |
Lens focal length | 8.8 mm |
Orientation | Normal |
Horizontal resolution | 350 dpi |
Vertical resolution | 350 dpi |
Software used | DSC-RX100M3 v1.20 |
File change date and time | 14:17, 24 February 2021 |
Y and C positioning | Centered |
Exposure Program | Normal program |
Exif version | 2.3 |
Date and time of digitizing | 14:17, 24 February 2021 |
Meaning of each component |
|
Image compression mode | 2 |
APEX brightness | 4.48203125 |
APEX exposure bias | 0 |
Maximum land aperture | 1.6953125 APEX (f/1.8) |
Metering mode | Pattern |
Light source | Unknown |
Flash | Flash did not fire, compulsory flash suppression |
DateTime subseconds | 000 |
DateTimeOriginal subseconds | 000 |
DateTimeDigitized subseconds | 000 |
Supported Flashpix version | 1 |
Color space | sRGB |
File source | Digital still camera |
Scene type | A directly photographed image |
Custom image processing | Normal process |
Exposure mode | Auto exposure |
White balance | Auto white balance |
Digital zoom ratio | 1 |
Focal length in 35 mm film | 24 mm |
Scene capture type | Standard |
Contrast | Normal |
Saturation | Normal |
Sharpness | Normal |
Lens used | Sony 24-70mm F1.8-2.8 |
IIM version | 2 |