Mar 6, 2023 16:01
1 yr ago
15 viewers *
English term
envelope of the box
English to Polish
Science
Astronomy & Space
It is assumed that the payload is a closed box containing the board described in 2.2. The maximum envelope of the box shall be 0.3 U.
Zapis z dokumentu pt. "Payload Mission Customization Scope of Work". Chodzi o wysłanie komputera pokładowego na niską orbitę okołoziemską.
Zapis z dokumentu pt. "Payload Mission Customization Scope of Work". Chodzi o wysłanie komputera pokładowego na niską orbitę okołoziemską.
Proposed translations
(Polish)
| 4 | największy wymiar pudełka |
Andrzej Mierzejewski
|
| 2 | obudowa boksu |
Frank Szmulowicz, Ph. D.
|
References
| payload envelope |
geopiet
|
Change log
Mar 6, 2023 16:19: M.A.B. changed "Field" from "Other" to "Science"
Proposed translations
17 hrs
Andrzej Mierzejewski
Poland
Poland
Native in Polish
Poland
M.Sc. Engineer (Mechanics)
Native in: Polish
Works in: Polish to English, English to Polish, German to Polish, and 3 more.
Related KudoZ points
:
7
Selected
największy wymiar pudełka
Propozycja na podstawie referencji podanych przez geopieta.
3 KudoZ points awarded for this answer.
Comment: "Dziękuję"
5 hrs
Frank Szmulowicz, Ph. D.
United States
United States
Native in English
&
Polish
United States
On time, on target, on budget.
Native in: English 
, Polish
Works in: Polish to English, English to Polish, Russian to Polish, and 1 more.
Related KudoZ points
:
9
obudowa boksu
Tak wynika z kontekstu.
Note from asker:
| Dziękuję |
Reference comments
8 hrs
Reference:
payload envelope
Payload Envelope
As a standard, RS1 uses a metallic, milled 80-inch (2.032m) diameter bi-conic fairing to shield the payload from aerodynamic buffeting and heating during ascent. The fairing is provisioned with acoustic protection provisions with ample clearance for dynamic movement of the fairing and payloads during the ascent. The fairing is a two-part assembly and separates along a longitudinal seam using low shock pneumatic and fully testable actuators. - https://ablspacesystems.com/wp-content/uploads/2022/06/ABL-P... - page 11
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DO NOT DESIGN TO THE LIMITS OF THE ENVELOPE.
The CDS defines the standard CubeSat “envelope”—that is to say, the length, height, and width dimensions of the CubeSat body—very specifically. It’s extremely important that your CubeSat measurements fall within the tolerances set in the CDS. If your CubeSat doesn’t fit, it doesn’t fly. - https://www.nasa.gov/sites/default/files/atoms/files/nasa_cs... - page 24
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4.4.1 Long Duration Captive Carry
The maximum envelope shown in Figure 4-7 is not constant during a Pegasus mission. The actual flight random vibration levels vary considerably throughout each phase of the Pegasus flight and are typically well below the maximum levels. - https://www.mach5lowdown.com/wp-content/uploads/PUG/pegasus-... - page 32
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4.1.4 Allowed Envelope
Figure 4.1.4-1 and 4.1.4-2 show the dynamic envelope of the two slide table configurations as based on the dimensions and diagrams from NASDA-ESPC-2903-B. Note that these represent the maximum dynamic envelope. The payload should designed to be no closer than one inch from the maximum envelope dimensions shown. NanoRacks will perform the mission dynamic analysis to help verify the envelope requirements. - https://nanoracks.com/wp-content/uploads/Nanoracks-Kaber-Dep... - page 25
As a standard, RS1 uses a metallic, milled 80-inch (2.032m) diameter bi-conic fairing to shield the payload from aerodynamic buffeting and heating during ascent. The fairing is provisioned with acoustic protection provisions with ample clearance for dynamic movement of the fairing and payloads during the ascent. The fairing is a two-part assembly and separates along a longitudinal seam using low shock pneumatic and fully testable actuators. - https://ablspacesystems.com/wp-content/uploads/2022/06/ABL-P... - page 11
---
DO NOT DESIGN TO THE LIMITS OF THE ENVELOPE.
The CDS defines the standard CubeSat “envelope”—that is to say, the length, height, and width dimensions of the CubeSat body—very specifically. It’s extremely important that your CubeSat measurements fall within the tolerances set in the CDS. If your CubeSat doesn’t fit, it doesn’t fly. - https://www.nasa.gov/sites/default/files/atoms/files/nasa_cs... - page 24
---
4.4.1 Long Duration Captive Carry
The maximum envelope shown in Figure 4-7 is not constant during a Pegasus mission. The actual flight random vibration levels vary considerably throughout each phase of the Pegasus flight and are typically well below the maximum levels. - https://www.mach5lowdown.com/wp-content/uploads/PUG/pegasus-... - page 32
---
4.1.4 Allowed Envelope
Figure 4.1.4-1 and 4.1.4-2 show the dynamic envelope of the two slide table configurations as based on the dimensions and diagrams from NASDA-ESPC-2903-B. Note that these represent the maximum dynamic envelope. The payload should designed to be no closer than one inch from the maximum envelope dimensions shown. NanoRacks will perform the mission dynamic analysis to help verify the envelope requirements. - https://nanoracks.com/wp-content/uploads/Nanoracks-Kaber-Dep... - page 25
Discussion
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"payload envelope" widoczna na rys. 11 - https://www.semanticscholar.org/paper/Space-access-for-small...
O znaczenie "envelope of the box" zapytałbym najpierw klienta (może już wie z wcześniejszej korespondencji), a następnie autora dokumentu.
BTW sugeruję nie usiłować przeliczania 0.3 U na milimetry, lecz tylko zamienić kropkę na przecinek.