درباره ما
MSFC-STD-3535
Standard for Propellants and Pressurants used for Test and Test Support Activities at SSC and MSFC
Organization:
MSFC - NASA - MSFC - Marshall Space Flight Center
Year: 2009
Abstract: PURPOSE
The purpose of this standard is to specify the minimum requirements for the certification and maintenance of propellant and pressurant (P/P) systems used for the purpose of rocket engine testing, test operations, ground support operations, center laboratory operations, and center facility operations.
APPLICABILITY
This standard is applicable to ground-based rocket propulsion test, test support, center sample analysis laboratory, and center operation facilities for P/P requiring system certification. P/P quality provided to the user interface points shall meet or exceed program, test article, center or laboratory requirements. Programs or customers may impose additional requirements. In such cases, process changes and supplemental procedures may be required.
Propellants and pressurants covered in this standard are high purity air (HPA), gaseous nitrogen (GN2), liquid nitrogen (LN2), gaseous hydrogen (GH), liquid hydrogen (LH), gaseous oxygen (GOX), liquid oxygen (LOX), gaseous helium, and liquid helium, and breathing air.
The purpose of this standard is to specify the minimum requirements for the certification and maintenance of propellant and pressurant (P/P) systems used for the purpose of rocket engine testing, test operations, ground support operations, center laboratory operations, and center facility operations.
APPLICABILITY
This standard is applicable to ground-based rocket propulsion test, test support, center sample analysis laboratory, and center operation facilities for P/P requiring system certification. P/P quality provided to the user interface points shall meet or exceed program, test article, center or laboratory requirements. Programs or customers may impose additional requirements. In such cases, process changes and supplemental procedures may be required.
Propellants and pressurants covered in this standard are high purity air (HPA), gaseous nitrogen (GN2), liquid nitrogen (LN2), gaseous hydrogen (GH), liquid hydrogen (LH), gaseous oxygen (GOX), liquid oxygen (LOX), gaseous helium, and liquid helium, and breathing air.
Collections
:
Show full item record
| contributor author | MSFC - NASA - MSFC - Marshall Space Flight Center | |
| date accessioned | 2017-09-04T18:22:20Z | |
| date available | 2017-09-04T18:22:20Z | |
| date copyright | 04/08/2009 | |
| date issued | 2009 | |
| identifier other | IAYQLCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho1216AF679D40527318548F1EFDEC014A/handle/yse/204734 | |
| description abstract | PURPOSE The purpose of this standard is to specify the minimum requirements for the certification and maintenance of propellant and pressurant (P/P) systems used for the purpose of rocket engine testing, test operations, ground support operations, center laboratory operations, and center facility operations. APPLICABILITY This standard is applicable to ground-based rocket propulsion test, test support, center sample analysis laboratory, and center operation facilities for P/P requiring system certification. P/P quality provided to the user interface points shall meet or exceed program, test article, center or laboratory requirements. Programs or customers may impose additional requirements. In such cases, process changes and supplemental procedures may be required. Propellants and pressurants covered in this standard are high purity air (HPA), gaseous nitrogen (GN2), liquid nitrogen (LN2), gaseous hydrogen (GH), liquid hydrogen (LH), gaseous oxygen (GOX), liquid oxygen (LOX), gaseous helium, and liquid helium, and breathing air. | |
| language | English | |
| title | MSFC-STD-3535 | num |
| title | Standard for Propellants and Pressurants used for Test and Test Support Activities at SSC and MSFC | en |
| type | standard | |
| page | 42 | |
| status | Active | |
| tree | MSFC - NASA - MSFC - Marshall Space Flight Center:;2009 | |
| contenttype | fulltext |