國家科技進步二等獎；全軍科技進步二等獎、三等獎（2次）；工信部一等獎；航空航天部科技進步三等獎（2次）；兵工部科技進步三等獎（2次）；海軍等其他省部級獎勵若幹……
[1]主編國家出版基金項目專著《發射氣體動力學》；
[2]主編國家出版基金項目專著《發射動力學》；
1 Inhibition Effect of Water Injection on Afterburning of Rocket Motor Exhaust Plume 中國航空學報（英文版） 姜毅；馬豔麗；王偉臣；邵立武 2010 SCI、EI
2 艦載導彈垂直發射系統燃氣流場的三維數值計算 伟德客户端學報 姜毅 2002 核心
3 雙噴管火箭發動機燃氣流場的三維數值計算與試驗 伟德客户端學報 姜毅；劉琪；王剛 2002 核心
4 機載導彈發射時燃氣流場的數值 彈箭與制導學報 姜毅；張曉琳；劉琪 2002 核心
5 沖壓式舵機腔内工作壓力随飛行速度變化規律的數值仿真 兵工學報 姜毅；劉琦；張曉琳 2004 EI
6 斜噴管燃氣射流氣動幹擾數值模拟 宇航學報 傅德彬；姜毅；張傑 2004 EI
7 燃氣射流氣固兩相數值模拟與顆粒沖刷分析 彈箭與制導學報 傅德彬；姜毅 2004 核心
8 燃氣射流氣固兩相流場研究 伟德客户端學報 傅德彬；姜毅；袁增鳳 2004 EI
9 同心筒自力發射燃氣排導優化設計 彈箭與制導學報 傅德彬；姜毅；陳建偉；劉琦 2004 核心
10 發射裝置剛柔耦合仿真分析 彈箭與制導學報 傅德彬；姜毅；劉琦 2004 核心
11 燃氣射流對發射車輪胎作用仿真 彈箭與制導學報 劉群；姜毅；郝繼光；傅德彬 2005 核心
12 燃氣流作用對車載箱式發射的動力學影響 導彈與航天運載技術 傅德彬；姜毅；劉琦 2006 核心
13 導彈頭部氣動加熱的流固耦合數值模拟 彈箭與制導學報 郝繼光；姜毅；劉琦 2006 核心
14 同心筒垂直發射裝置排導燃氣流的改進 伟德客户端學報 姜毅；郝繼光 2007 EI
15 用動網格方法模拟導彈發射過程中的燃氣射流流場 宇航學報 傅德彬；姜毅 2007 EI
16 一種新的動網格更新技術及其應用 彈道學報 郝繼光；姜毅； 韓書永; 廖慶 2007 EI
17 液壓系統半實物仿真平台設計 系統仿真學報 傅德彬；姜毅； 張強 2007 EI
18 燃氣射流對發射車天線影響分析 彈箭與制導學報 劉群；姜毅；郝繼光 2007 EI
19 某導彈易碎蓋的開啟過程 固體火箭技術 傅德彬；姜毅 2007 EI
20 Compensator design for aspheric testing using virtual glass model 3rd International Symposium on Advanced Optical Manufacturing and Testing Technologies 姜毅；王萍；齊月靜；魏楠 2007 EI
21 某型導彈發動機推進劑惡劣工況下溫度仿真研究 兵工學報 劉群；姜毅；郝繼光 2007 EI
22 基于FPGA的非标準二次群路的分接處理 2007儀表、自動化及先進集成技術大會論文集 姜毅；齊月靜 2008 EI
23 新型“引射同心筒”垂直發射裝置理論及試驗研究 宇航學報 姜毅；郝繼光；傅德彬；耿峰 2008 EI
24 導彈發動機推進劑惡劣工況下溫度分析 中北大學學報 姜毅；王豔彬；劉群 2008 EI
25 液壓系統半實物仿真通信過程實施 系統仿真學報 傅德彬；姜毅；張強 2008 EI
26 固體火箭發動機尾噴焰複燃流場計算 宇航學報 姜毅；傅德彬 2008 EI
27 導彈發射過程三維非定常數值模拟 兵工學報 姜毅；郝繼光；傅德彬 2008 EI
28 導彈發射筒蓋開啟過程數值計算及試驗 彈道學報 姜毅；耿峰；張強 2008 EI
29 基于剛柔耦合模型的發射裝置動力學仿真分析 系統仿真學報 傅德彬；姜毅 2009 EI
30 基于MSDM方法的粒子-固壁侵蝕效應研究 固體火箭技術 傅德彬；姜毅 2009 EI
31 Numerical simulation of the erecting system for large device 2009 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2009 姜毅；張強；傅德彬；席運陽 2009 EI
32 基于容腔節點法的液壓起豎系統仿真 機床與液壓 張強；姜毅；傅德彬；席運陽 2010 核心
33 某低空低速飛行器氣動特性計算 戰術導彈技術 馬豔麗；姜毅；郝繼光 2010 核心
34 固體發動機燃氣射流對發射平台沖擊效應研究 固體火箭技術 馬豔麗；姜毅；郝繼光；趙剛練 2010 EI
35 濕式同心筒自力垂直熱發射技術降溫效果研究 彈道學報 馬豔麗；姜毅；王偉臣；顔鳳；郝繼光 2010 EI
36 Optimization design of the rocket launching facilities and the thermal protection 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010 姜毅；馬豔麗；王偉臣；郝繼光 2010 EI
37 伟德客户端學報（英文版） 馬豔麗；姜毅；郝繼光；劉伯偉 2010 EI
38 濕式獨立自排導垂直發射技術研究 導彈與航天運載技術 馬豔麗；姜毅；王偉臣；劉伯偉；顔鳳 2011 核心
39 同心筒發射過程燃氣射流沖擊效應研究 固體火箭技術 馬豔麗；姜毅；王偉臣；郝繼光；趙剛練 2011 EI
40 固體火箭發動機尾焰注水流場實驗研究 彈箭與制導學報 姜毅；周帆；張學文 2011 EI
41 艦載導彈垂直彈射出筒姿态影響因素分析 彈箭與制導學報 陳餘軍；姜毅 2011 EI
42 炮射導彈氣動特性數值計算 伟德客户端學報 郭慶陽；姜毅；郭利強；石庚辰 2011 EI
43 噴水對火箭發動機羽流紅外特性的抑制作用研究 伟德客户端學報 馬豔麗；姜毅；王偉臣；郝繼光；趙剛練 2011 EI
44 新型艦載同心筒發射過程流場研究 導彈與航天運載技術 邵立武；姜毅；馬豔麗；王偉臣 2011 核心
45 超聲速高溫沖擊射流注水流場實驗研究 實驗流體力學 姜毅；周帆；張學文 2011 EI
46 含側噴流炮射導彈繞流場數值計算 伟德客户端學報 郭慶陽；姜毅；于天朋；石庚辰 2011 EI
47 艦載導彈發射數值模拟與點火時機研究 固體火箭技術 陳餘軍；姜毅；趙剛練 2011 EI
48 車載導彈行進間發射動力學仿真 彈箭與制導學報 陳餘軍；姜毅 2011 EI
49 Simulation and optimize design for deflector plate of the Vehicle mounted Vertically Thermal Launched missile Advanced Materials Research 于邵祯；姜毅；馬豔麗；馬豔豔；劉伯偉 2012 EI
50 火箭發動機尾焰流場注水降溫效果初探 推進技術 周帆；姜毅；郝繼光 2012 EI
51 基于有限狀态機的多級液壓缸仿真分析 機床與液壓 邵立武；姜毅；傅德彬；馬豔豔 2012 核心
52 車載導彈發射過程姿态模拟 彈道學報 陳餘軍；姜毅； 2012 EI
53 Parametric design of parts in an integrated simulation system based on asynchronous mode of pro/TOOLKIT Advanced Mechanical Design 趙剛練；姜毅；陳餘軍；馬豔麗 2012 EI
54 Research on the jet influence on the mechanical launcher of various ignition height Lecture Notes in Electrical Engineering 賀衛東；姜毅；馬豔麗 2012 EI
55 Study on the deployment process of low attitude interception net Advances in Intelligent and Soft Computing 周笑飛；姜毅；李永遠 2012 EI
56 Numerical simulation on the influence of altitude on jet flow field Lecture Notes in Electrical Engineering 劉伯偉；姜毅；宋洋；于邵祯 2012 EI
57 Optimization design for launch box based on the effect of the shock wave Lecture Notes in Electrical Engineering 于邵祯；姜毅；鄧佳；劉伯偉；趙剛練 2012 EI
58 Study on the Firing Table Compiling of a new type of the very low altitude interception device Advanced Research on Engineering Materials, Energy, Management and Control 鐘洲；姜毅；李永遠；張沖 2012 EI
59 火箭發動機射流複雜噪聲測量數據時頻分析 彈箭與制導學報 周帆；姜毅；張學文；郝繼光 2012 EI
60 A new method of integrate simulation based on ADAMS and pro/ENGINEER 4th International Conference on Mechanical and Electrical Technology, ICMET 2012 趙剛練；姜毅；陳餘軍；馬豔麗 2012 EI
61 Analysis of concentric canister wall roughness effect on jet flow based on fluid dynamics 2012 International Conference on Applied Mechanics and Manufacturing System, AMMS 2012 拜雲山；姜毅；周東默 2013 EI
62 Research on the initial disturbance of vehicular missile with system vibration analysis 2012 International Conference on Mechanics, Dynamic Systems and Material Engineering, MDSME 2012 張沖；姜毅 2013 EI
63 Launching dynamics simulation of ship-board rocket gun 2012 International Conference on Mechanics, Dynamic Systems and Material Engineering, MDSME 2012 曾偉；姜毅 2013 EI
64 Mechanics analysis with different open lid time on shockwaves in launch box 2013 3rd International Conference on Automation, Communication, Architectonics and Materials, ACAM 2013 曹全峥；姜毅；楊征然；于邵祯 2013 EI
65 Deflecting features of gas from double-faced deflector and structure optimization of deflector 2013 International Conference on Applied Mechanics, Materials and Mechanical Engineering, AMME 2013 史少岩；姜毅；董曉彤 2013 EI
66 Failure analysis of a composite frangible cover based on transient dynamics 3rd International Conference on Advanced Design and Manufacturing Engineering, ADME 2013 曾偉；姜毅 2013 EI
67 間接法求解具有最大橫程的再入軌迹 伟德客户端學報 李永遠；姜毅;；高偉濤；黃春平 2013 EI
68 考慮導軌間隙的在軌分離動力學計算方法 力學學報 趙剛練；姜毅；陳餘軍；董曉彤 2013 EI
69 考慮圓柱鉸鍊間隙的多剛體系統動力學計算方法 振動與沖擊 趙剛練；姜毅；郝繼光；陳餘軍；龔俊斌 2013 EI
70 汽化效應對燃氣蒸汽式彈射氣液兩相流場的影響 固體火箭技術 劉伯偉；姜毅 2013 EI
71 基于遺傳算法的導彈發射系統設計參數優化 彈箭與制導學報 曾偉；姜毅 2013 核心
72 車載防空導彈行進發射過程動力學數值分析 兵工學報 鐘洲；姜毅；劉群 2013 EI
73 基于FFT算法的艦載導彈發射彈位研究 振動與沖擊 鐘洲；姜毅 2013 EI
74 Dynamic simulation analysis of shipborne missile launching under high-wave-level environment 2012 International Conference on Advanced Materials Design and Mechanics, ICAMDM 2012 鐘洲；姜毅；李永遠；張沖 2013 EI
75 導軌排氣孔對發射箱内流場影響的計算分析 固體火箭技術 牛钰森；姜毅；史少岩 2013 EI
76 撓性航天器在軌分離沖擊緩沖模糊滑模控制研究 固體火箭技術 趙剛練；姜毅；陳餘軍；劉冬 2013 EI
77 An improved rollover index based on BP neural network for hydropneumatic suspension vehicles,MATHEMATICAL PROBLEMS IN ENGINEERING. 文獻号: 7859521 DOI: 10.1155/2018/7859521 出版年: 2018
78 Detection Probability for Moving Ground Target of Normal Distribution Using an Imaging Satellite.CHINESE JOURNAL OF ELECTRONICS 卷: 27 期: 6 頁: 1309-1315 DOI: 10.1049/cje.2018.08.005 出版年: NOV 2018
79 Rollover threshold investigation of a heavy-duty vehicle during cornering based on multi-body dynamics. ADVANCES 80 IN MECHANICAL ENGINEERING卷: 10 期: 7 文獻号: 1687814018789505 DOI: 10.1177/1687814018789505 出版年: JUL 19 2018
81 The Impact of Concrete Pavement Field Floor to Vehicle Missile Launching Process. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING 文獻号: 1624107 DOI: 10.1155/2017/1624107 出版年: 2017
82 The coupling effects of the missile launcher and the ground in vehicle-mounted missile erecting. ADVANCES IN MECHANICAL ENGINEERING 卷: 8 期: 7 文獻号: 1687814016656106 DOI: 10.1177/1687814016656106 出版年: JUL 2016
83 Cooling Effect of Water Injection on a High-Temperature Supersonic Jet. ENERGIES 卷: 8 期: 11 頁: 13194-13210 DOI: 10.3390/en81112363 出版年: NOV 2015
84 Mobile Network Computer Can Better Describe The Future of Information Society. CHINA COMMUNICATIONS 卷: 13 期: 12 頁: 90-96 DOI: 10.1109/CC.2016.7897558 出版年: DEC 2016
85 Mobile Network Computers Should be the Terminal of Mobile Communication Networks. WIRELESS PERSONAL COMMUNICATIONS 卷: 85 期: 4 頁: 1895-1904 DOI: 10.1007/s11277-015-2878-0 出版年: DEC 2015
86 Research on the Simulation Method of Missile Adapter's Separation Based on Combined Calculation. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING 文獻号: 9804190 DOI: 10.1155/2019/9804190 出版年: 2019
87 Horizontal Backward Launch Dynamics Modeling and Analysis. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING 文獻号: 4098398 DOI: 10.1155/2019/4098398 出版年: 2019
88 Assessing Turbulence Models on the Simulation of Launch Vehicle Base Heating. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING 文獻号: 1624107 DOI: 10.1155/2019/1624107 出版年: 2019
89 The effect of thrust eccentric and erection cylinder anchor position on the initial disturbances. Advanced Materials Research, v 889-890, p 165-169, 2014
90 Analysis of a missile's initial disturbance. Advanced Materials Research, v 889-890, p 152-155, 2014
Coupling of missile-launcher in vertical thermal launch process. Zhendong yu Chongji/Journal of Vibration and Shock, v 33, n 1, p 89-94, January 15, 2014
91 Study on the cooling effect of water injection on flame of vertical launch system. Guti Huojian Jishu/Journal of Solid Rocket Technology, v 38, n 5, p 628-634, October 1, 2015
92 Numerical analysis of fragile back cover opening process coupling with jet flow. Binggong Xuebao/Acta Armamentarii, v 36, n 1, p 87-93, January 1, 2015
93 Dynamics numerical analysis of vehicle-mounted antiaircraft missile launching on the move. Binggong Xuebao/Acta Armamentarii, v 35, n 1, p 83-87, January 2014
94 Analysis on the effect of shipborne missile launch position based on fast Fourier transform. Zhendong yu Chongji/Journal of Vibration and Shock, v 33, n 13, p 210-214, July 15, 2014
95 Numerical calculation on the influence of missile exhaust plume with mechanical properties to the double-launch box. Advanced Materials Research, v 978, p 101-105, 2014
96 Influence of vaporization effect on gas-liquid two-phase flow field of ejection in combustion gas and vapor mode. Guti Huojian Jishu/Journal of Solid Rocket Technology, v 37, n 2, p 156-160, April 2014
97 Calculation and analysis about the impact of guide vents on the flow field inside the launching canister. Guti Huojian Jishu/Journal of Solid Rocket Technology, v 37, n 2, p 161-166, April 2014
98 Research on Efficiency of Additional Thrust of Thermal Launching. Binggong Xuebao/Acta Armamentarii, v 37, n 6, p 1038-1043, June 10, 2016
99 Effect of Rocket Engine Jet Flow with Water Injection on Air-flow Exhaust of Gas-flow-guided Channel. Binggong Xuebao/Acta Armamentarii, v 38, n 1, p 97-105, January 13, 2017
100 Research on distribution of flow field in launching canister with the effect of nozzle closure. Binggong Xuebao/Acta Armamentarii, v 35, n 11, p 1805-1812, November 1, 2014
