真空与低温
真空與低溫
진공여저온
VACUUM AND CRYOGENICS
2014年
3期
154-157
,共4页
黄小琦%王立%刘宇飞%高鸿%王永建%田海%冯展祖%柳青
黃小琦%王立%劉宇飛%高鴻%王永建%田海%馮展祖%柳青
황소기%왕립%류우비%고홍%왕영건%전해%풍전조%류청
太阳帆%聚酰亚胺薄膜%电子辐照%力学性能
太暘帆%聚酰亞胺薄膜%電子輻照%力學性能
태양범%취선아알박막%전자복조%역학성능
solar sail%polyimide film%electron irradiation%mechanical performance
太阳帆是十分有利于深空探测的一种新型飞行器,帆面采用超轻薄的薄膜材料,提高飞行器的推进性能。帆面材料长期暴露在空间,由于长期受到空间粒子辐射环境的影响,性能发生退化影响在空间的应用。研究空间电子与薄膜相互作用的机理,分析电子沉积剂量,通过地面模拟不同剂量的空间电子辐照环境,对辐照后新型超薄帆面材料力学性能的研究,满足太阳帆在空间应用要求。结果表明:超薄聚酰亚胺薄膜材料,在厚度及辐照力学性能得到了较大的突破,但断裂伸长率仍需提升,电子辐照后性能略有下降,耐辐照性能也需进一步提高。
太暘帆是十分有利于深空探測的一種新型飛行器,帆麵採用超輕薄的薄膜材料,提高飛行器的推進性能。帆麵材料長期暴露在空間,由于長期受到空間粒子輻射環境的影響,性能髮生退化影響在空間的應用。研究空間電子與薄膜相互作用的機理,分析電子沉積劑量,通過地麵模擬不同劑量的空間電子輻照環境,對輻照後新型超薄帆麵材料力學性能的研究,滿足太暘帆在空間應用要求。結果錶明:超薄聚酰亞胺薄膜材料,在厚度及輻照力學性能得到瞭較大的突破,但斷裂伸長率仍需提升,電子輻照後性能略有下降,耐輻照性能也需進一步提高。
태양범시십분유리우심공탐측적일충신형비행기,범면채용초경박적박막재료,제고비행기적추진성능。범면재료장기폭로재공간,유우장기수도공간입자복사배경적영향,성능발생퇴화영향재공간적응용。연구공간전자여박막상호작용적궤리,분석전자침적제량,통과지면모의불동제량적공간전자복조배경,대복조후신형초박범면재료역학성능적연구,만족태양범재공간응용요구。결과표명:초박취선아알박막재료,재후도급복조역학성능득도료교대적돌파,단단렬신장솔잉수제승,전자복조후성능략유하강,내복조성능야수진일보제고。
Solar sail is a new kind of spacecraft for deep space exploration.The ultra lightweight and thin membrane material are used to promote the spacecraft propulsion.Solar sail would stay in space for a long time, and the performance of sail membrane would decrease under the influence of the space radiation .The interaction mechanism between electron and sail material is discussed.Also, radiation dose that deposited in material by electrons is analyzed.After exposure to different electron radiation doses, the mechanical are investigated and their ability to meet demand for space applications is analyzed. Result shows that ultra thin polyimide film get a great accomplishment in thickness and mechanical properties before its expo-sure to electrons, but the elongation before break still need a promotion.Mechanical performance has decreased after electron exposure, and improvement in irradiation-resistance is also needed.