欢迎登录材料期刊网

材料期刊网

高级检索

Re/Ir发动机是美国研制成功的应用于空间飞行器的第三代高性能发动机.作者对Re/Ir发动机的核心部件-Re/Ir喷管研究的国内外进展进行了简要的评述,内容包括:Re和Ir的性能;Re和Ir的CVD制备;Re/Ir喷管的制备;Re/Ir喷管的连接以及发动机工作寿命等.

参考文献

[1] Harding J T;Tuffias R H;Kaplan R B.Oxidation resistant coatings for refractory metals[A].Laurel MD:CPIA Publication,1985:181-188.
[2] Harding J T;Fry V R.Oxidation protection of refractory materials by CVD coatings of iridium and other platinum group metals[A].Lake tahoe,Nevada:International Precious Metals Institute,1986:431-437.
[3] Harding J T;Kazaroff J M;Appel M A .Iridium-coated rhenium thrusters by CVD[NASA TM-101309][R].,1988.
[4] Wooten J R;Lansaw P T .High-temperature,oxidation-resistant thruster research[NASA CR-185233][R].,1990.
[5] Schoenman L;Rosenberg S D;Jassowski D M .Test experience,490-N high-performance[321-s Specific Impulse] engine[J].Journal of Propulsion and Power,1995,11(05):992.
[6] Jassowski D M .Advanced small rocket chambers basic program and option II-Fundamental progresses and material evaluation[NASA CR-195349][R].,1993.
[7] Jassowski D M;Schoenman L .Advanced small rocket chambers option3-110 lbf (490N) Ir-Re rocket[NASA CR-195435][R].,1995.
[8] Fortini A J;Tuffias R H .Advanced materials for chemical propulsion:oxide-iridium/rhenium combustion chambers[AIAA 99-2894][R].,1999.
[9] Jassowski D M;Gage M L .Advanced small rocket chambers option1-14 Lbf Ir-Re rocket[NASA CR-191014][R].,1992.
[10] Wood R S.Experiences with high temperature materials for small thrusters[AIAA 93-1962][A].Monterey,California,USA,1993
[11] Changguo Liu;Jie Chen;Hongyin Han;Yunwu Wang;Zhongguang Zhang .A long duration and high reliability liquid apogee engine for satellites[J].Acta astronautica,2004(3/9):401-408.
[12] 小推力姿/轨控液体火箭发动机材料的研究进展[J].宇航材料工艺,2005(05):11-15.
[13] Wimber R T;Kraus H G.Oxidation of Iridium[J].Metallurgical Transactions,1974(05):1565-1572.
[14] Wimber R T;Hills S W;Wahl N K.Kinetics of evaporation/oxidation of iridium[J].Metallurgical and Materials Transactions A:Physical Metallurgy and Materials Science,1977(8A):193-199.
[15] Jehn H .High temperature behavior of platinum group metals in oxidizing atmospheres[J].JOURNAL OF THE LESS-COMMON METALS,1984,100(321-329)
[16] Gulbransen E A;Brassart F A.Oxidation of rhenium and a rhenium-8% titanium alloy in flow environments at oxygen pressures of 1-10 torr and 800-1400℃[J].JOURNAL OF THE LESS-COMMON METALS,1968(14):17.
[17] Reed B D.High temperature oxidation behavior of iridium-rhenium alloys[A].,1994
[18] Biaglow J A .Rhenium material properties[AIAA 95-2398][R].,1995.
[19] Mittendorf D .The effect of manufacturing processes on the mechanical integrity of rhenium[AIAA 97-2675][R].,1997.
[20] Jassowski D M;Gage M L .Advanced small rocket chambers option1-14 Lbf Ir-Re rocket[NASA CR-191014][R].,1992.
[21] Falce L R .Iridium cathode development[N00713-77-C-0186][R].,1978.
[22] Schneider J S.High-temperature thruster technology for spacecraft propulsion[A].Montreal,Canada,1991
[23] Federer J I;Schaffhauser.Chemical vapor deposition and characterization of tungsten-rhenium alloys[A].USA,1979:242-252.
[24] Sherwood P J.The relation between the Mechanical properties and the microstructure of chemically vapor deposition (CVD) tungsten and rhenium[A].USA,1978:728-739.
[25] Yang L;Hudson R G;Ward J J.Preparation and evaluation of chemical vapor deposition rhenium thermionic emitters[A].Salt Lake City,Utah,USA,1972:253-267.
[26] Donaldson J G;Hoertel F W;Cochran A A .A preliminary study of vapor deposition of rhenium and rhenium-tungsten[J].JOURNAL OF THE LESS-COMMON METALS,1968,14:93-101.
[27] Reed B D.Rocket screening of iridium/rhenium[A].Cleveland OH,1998
[28] Toenshoff D A;Lanam R D;Ragaini J.Iridium coated rhenium rocket chambers produced by electroforming[A].Huntsville Alabama,2000
[29] Lanam R D;Shchetkovskiy A;Smirnov A.Properties and enhanced capabilities for EL-FormTM rhenium[A].Salt Lake City,Utah,USA,2001
[30] Tuffias R H;Brockmeyer J W;Fortini A J.Engineering issues of iridium /rhenium rocket engines revisited[M].Los Angeles,California,USA,1999
[31] Reed B D;Biaglow J A.Rhenium mechanical properties and joining technology[A].Lake Buena,Vista,FL,1996
[32] Stechman C;Woll P;Fuller R et al.A high performance liquid rocket engine for satellite main propulsion[AIAA 2000-3161][R].,2000.
[33] Hamilton J C;Yang N Y C;Clift W M et al.Diffusion mechanisms in iridium-coated rhenium for high-temperature,radiation-cooled rocket thrusters[AIAA91-2215:][R].,1991.
[34] 胡昌义,陈松,杨家明,邓德国,高逸群,尹志民,王云,李靖华.CVD法制备的Ir/Re涂层复合材料界面扩散研究[J].稀有金属材料与工程,2003(10):796-798.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%