Development of an Advanced Rocket Propellant Handler's Suit

by donald F.doerr; Chief Biomedical engineering; Nasa

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Development of an Advanced Rocket Propellant Handler's Suit

机译：先进的火箭推进剂处理者服的研制

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Most launch vehicles and satellites in the US inventory rely upon the use of hypergolic rocket propellants, many of which are toxic to humans. These fuels and oxidizers, such as hydrazine and nitrogen tetroxide have threshold limit values as low as 0.01 PPM> It is essential to provide space workers handling these agents whole body protection as they are universally hazardous not only to the respiratory system. But the skin as well.

机译：美国库存中的大多数运载火箭和卫星都依赖使用高定性火箭推进剂，其中许多对人类有毒。这些燃料和氧化剂（例如肼和四氧化二氮）的阈值极限值低至0.01 PPM>必须为处理这些药剂的航天员提供全身保护，因为它们不仅普遍危害呼吸系统。但是皮肤也是如此。

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《Acta astronautica》 |2001年第10期|p.463-468|共6页
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by donald F.doerr; Chief Biomedical engineering; Nasa;
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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航天（宇宙航行）;
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1. Improving the Mechanical Properties of Glycidyl Azide Polymeric Matrix Used in Composite Solid Rocket Propellant by Adding Advanced Cross‐Linker [J] . Boshra Islam K., Elbeih Ahmed, Mostafa Hosam E. Zeitschrift fur Anorganische und Allgemeine Chemie . 2019,第5期

机译：通过添加先进的交联剂，改善复合固体火箭推进剂中使用的缩水甘油叠氮化物聚合物基质的力学性能
2. ADVANCED LIQUID AND GELLED PROPELLANTS FOR ROCKET AND RAMJET PROPULSION [J] . Helmut K. Ciezki, Michele Negri, Andreas Gernoth International journal of energetic materials and chemical propulsion . 2015,第2期

机译：用于火箭和RAMJET推进的高级液体和胶凝推进剂
3. NG PLASTICIZED PE-PCP BINDER-BASED ADVANCED SOLID ROCKET PROPELLANTS: STUDIES ON MECHANICAL PROPERTIES [J] . Shrikant M. Pande, Vaibhav S. Sadavarte, Debdas Bhowmik, International journal of energetic materials and chemical propulsion . 2012,第2期

机译：基于NG的PE-PCP粘结剂的高级固体火箭推进剂：力学性能研究
4. DEVELOPMENT OF A LIQUID PROPELLANT ROCKET, KOREA SOUNDING ROCKET (KSR)-III [C] . Yeon Seok Chae, Soo Yong Lee, Seongbyeon Seo International Symposium on Liquid Space Propulsion . 2005

机译：开发液体推进剂火箭，韩国发声火箭（KSR）-III
5. Axisymmetric expansion of an ionized propellant gas under the effect of magnetic fields in advanced rocket nozzle. [D] . Gonzalez Villarreal, Dora Elia. 1994

机译：先进火箭喷嘴中磁场作用下离子化推进剂气体的轴对称膨胀。
6. Examination of the liver in personnel working with liquid rocket propellant [O] . Palle Petersen, Erik Bredahl, Ove Lauritsen, 1970

机译：液体火箭推进剂工作人员的肝脏检查
7. ORBITEC Advanced Cryogenic Solid Hybrid Rocket Engine and Propellant Developments: A 1998 Status Report [O] . Eric E. Rice, Edward Bangsund, Martin J. Chiaverini, 1998

机译：Orbitec高级低温固体混合火箭发动机和推进剂发展：1998年状态报告
8. A Rocket Propellant Handler's Suit for Protection from Chlorine Trifluoride and Elemental Fluorine [R] . Martone, J. A., Bergen, G. A. 1971

机译：火箭推进剂处理器适用于防止三氟化氯和元素氟的保护

Development of an Advanced Rocket Propellant Handler's Suit

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