MSFC-RQMT-3182 REV A
DELTA-L EXPERIMENT REQUIREMENTS, VERIFICATION, & COMPLIANCE (RVC)
Organization:
MSFC - NASA - MSFC - Marshall Space Flight Center
Year: 2003
Abstract:
These requirements are the basis for a verification program that will yield compliance data to demonstrate that the Delta-L experiment satisfies performance, functionality, safety, and interface requirements. These verification requirements will ensure that the Delta-L experiment has the capability to perform mission objectives both safety and efficiently for launch on the STS-118 (13A.1) and STS-119 (15A). All components of the Delta-L experiment will be stowed in stowage foam in the SPACEHAB with the exception of the Fluid Assembly that will be transported to ISS via a Single-Locker Thermal Enclosure System (STES) located in the Shuttle Middeck. Once onboard the ISS, the Delta-L experiment will be installed in the Microgravity Science Glovebox (MSG) utilizing g-LIMIT for vibration isolation (if available) during experiment operations. In the event that g-LIMIT is unavailable, Delta-L will be operated inside the MSG with g-LIMIT by-pass cables if necessary. Delta-L requires the space of three Middeck Locker Equivalents (MDLE) of stowage volume. There are two Delta-L units used in this verification program: One flight unit and one flight/training unit. See Figure (1) for Delta-L Requirements Documentation Flow.
Verification activities include demonstration (functionality / performance), testing, inspection, and analysis, which will be conducted primarily at the Marshall Space Flight Center (MSFC).
PURPOSE
This document establishes an "end-to-end" verification program for the Delta-L project.
These requirements are the basis for a verification program that will yield compliance data to demonstrate that the Delta-L experiment satisfies performance, functionality, safety, and interface requirements. These verification requirements will ensure that the Delta-L experiment has the capability to perform mission objectives both safety and efficiently for launch on the STS-118 (13A.1) and STS-119 (15A). All components of the Delta-L experiment will be stowed in stowage foam in the SPACEHAB with the exception of the Fluid Assembly that will be transported to ISS via a Single-Locker Thermal Enclosure System (STES) located in the Shuttle Middeck. Once onboard the ISS, the Delta-L experiment will be installed in the Microgravity Science Glovebox (MSG) utilizing g-LIMIT for vibration isolation (if available) during experiment operations. In the event that g-LIMIT is unavailable, Delta-L will be operated inside the MSG with g-LIMIT by-pass cables if necessary. Delta-L requires the space of three Middeck Locker Equivalents (MDLE) of stowage volume. There are two Delta-L units used in this verification program: One flight unit and one flight/training unit. See Figure (1) for Delta-L Requirements Documentation Flow.
Verification activities include demonstration (functionality / performance), testing, inspection, and analysis, which will be conducted primarily at the Marshall Space Flight Center (MSFC).
PURPOSE
This document establishes an "end-to-end" verification program for the Delta-L project.
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MSFC-RQMT-3182 REV A
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| contributor author | MSFC - NASA - MSFC - Marshall Space Flight Center | |
| date accessioned | 2017-09-04T16:13:27Z | |
| date available | 2017-09-04T16:13:27Z | |
| date copyright | 37950 | |
| date issued | 2003 | |
| identifier other | SRTHFBAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/76762 | |
| description abstract | These requirements are the basis for a verification program that will yield compliance data to demonstrate that the Delta-L experiment satisfies performance, functionality, safety, and interface requirements. These verification requirements will ensure that the Delta-L experiment has the capability to perform mission objectives both safety and efficiently for launch on the STS-118 (13A.1) and STS-119 (15A). All components of the Delta-L experiment will be stowed in stowage foam in the SPACEHAB with the exception of the Fluid Assembly that will be transported to ISS via a Single-Locker Thermal Enclosure System (STES) located in the Shuttle Middeck. Once onboard the ISS, the Delta-L experiment will be installed in the Microgravity Science Glovebox (MSG) utilizing g-LIMIT for vibration isolation (if available) during experiment operations. In the event that g-LIMIT is unavailable, Delta-L will be operated inside the MSG with g-LIMIT by-pass cables if necessary. Delta-L requires the space of three Middeck Locker Equivalents (MDLE) of stowage volume. There are two Delta-L units used in this verification program: One flight unit and one flight/training unit. See Figure (1) for Delta-L Requirements Documentation Flow. Verification activities include demonstration (functionality / performance), testing, inspection, and analysis, which will be conducted primarily at the Marshall Space Flight Center (MSFC). PURPOSE This document establishes an "end-to-end" verification program for the Delta-L project. | |
| language | English | |
| title | MSFC-RQMT-3182 REV A | num |
| title | DELTA-L EXPERIMENT REQUIREMENTS, VERIFICATION, & COMPLIANCE (RVC) | en |
| type | standard | |
| page | 408 | |
| status | Active | |
| tree | MSFC - NASA - MSFC - Marshall Space Flight Center:;2003 | |
| contenttype | fulltext |

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