科技报告详细信息
Using a "HOLLoW" Design for Traditional Shuttle Tiles to Reduce Mass up to 30% | |
Peterson, Keith H ; Carder, Nichole B | |
关键词: PAYLOADS; TILES; RATIOS; SPACECRAFT DESIGN; MASS; LOW DENSITY MATERIALS; THERMAL RESISTANCE; | |
RP-ID : ARC-E-DAA-TN71614 | |
学科分类:航空航天科学 | |
美国|英语 | |
来源: NASA Technical Reports Server | |
【 摘 要 】
For spacecraft entering an atmosphere, a reduction in TPS mass is directly proportional to the increase in payload mass. The HOLLOW TPS concept is a reusable material with lower density and similar thermal capabilities to traditional tiles. Using HOLLOW TPS to replace a percentage of the tiles on a flight vehicle could save up to 35% mass depending on the mission objectives and flight path. The HOLLOW TPS will also increase an equal amount of payload capacity, increasing the efficiency of the mission.
【 预 览 】
Files | Size | Format | View |
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20190031965.pdf | 60KB | download |