16:01 Mar 6, 2023 |
English to Polish translations [PRO] Science - Astronomy & Space | |||||
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| Selected response from: Andrzej Mierzejewski Poland Local time: 19:21 | ||||
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Summary of answers provided | ||||
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4 | największy wymiar pudełka |
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2 | obudowa boksu |
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Summary of reference entries provided | |||
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payload envelope |
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Discussion entries: 8 | |
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obudowa boksu Explanation: Tak wynika z kontekstu. |
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Notes to answerer
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największy wymiar pudełka Explanation: Propozycja na podstawie referencji podanych przez geopieta. |
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8 hrs |
Reference: payload envelope Reference information: 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 --- 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 |
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