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                             70 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 A Chang’e-4 mission concept and vision of future Chinese lunar exploration activities Wang, Qiong
 2016
 127 C p. 678-683
6 p.
 artikel
2 A contribution to the definition of a new method to predict the catastrophic disintegration of spacecraft after collision with large orbital debris Zaccariotto, M.
 2016
 127 C p. 95-102
8 p.
 artikel
3 Adaptive control and orbit determination for elliptical rendezvous Xu, Lijia
 2016
 127 C p. 587-592
6 p.
 artikel
4 Adaptive sliding mode control of tethered satellite deployment with input limitation Ma, Zhiqiang
 2016
 127 C p. 67-75
9 p.
 artikel
5 Aero-thermo-dynamic analysis of a low ballistic coefficient deployable capsule in Earth re-entry Zuppardi, G.
 2016
 127 C p. 593-602
10 p.
 artikel
6 A multi-spacecraft formation approach to space debris surveillance Felicetti, Leonard
 2016
 127 C p. 491-504
14 p.
 artikel
7 A novel laser ablation plasma thruster with electromagnetic acceleration Zhang, Yu
 2016
 127 C p. 438-447
10 p.
 artikel
8 Application of a multi-objective evolutionary algorithm to the spacecraft stationkeeping problem Myers, Philip L.
 2016
 127 C p. 76-86
11 p.
 artikel
9 Application of particle damper on electronic packages for spacecraft Veeramuthuvel, P.
 2016
 127 C p. 260-270
11 p.
 artikel
10 Asteroid retrieval missions enabled by invariant manifold dynamics Sánchez, Joan Pau
 2016
 127 C p. 667-677
11 p.
 artikel
11 Circular revisit orbits design for responsive mission over a single target Li, Taibo
 2016
 127 C p. 219-225
7 p.
 artikel
12 Combustion-based power source for Venus surface missions Miller, Timothy F.
 2016
 127 C p. 197-208
12 p.
 artikel
13 Comparing long-term projections of the space debris environment to real world data – Looking back to 1990 Radtke, Jonas
 2016
 127 C p. 482-490
9 p.
 artikel
14 Computational investigation on combustion instabilities in a rocket combustor Yuan, Lei
 2016
 127 C p. 634-643
10 p.
 artikel
15 Constrained spacecraft reorientation using mixed integer convex programming Tam, Margaret
 2016
 127 C p. 31-40
10 p.
 artikel
16 Decentralized adaptive sliding mode control for beam synchronization of tethered InSAR system Zhang, Jinxiu
 2016
 127 C p. 57-66
10 p.
 artikel
17 Deployable Pipe-Z Zawidzki, Machi
 2016
 127 C p. 20-30
11 p.
 artikel
18 Did the Germans learn from Goddard? An examination of whether the rocketry of R.H. Goddard influenced German Pre-World-War II missile development Winter, Frank H.
 2016
 127 C p. 514-525
12 p.
 artikel
19 Dynamic modelling and stability parametric analysis of a flexible spacecraft with fuel slosh Gasbarri, Paolo
 2016
 127 C p. 141-159
19 p.
 artikel
20 Effect of vibration on two-liquid system in rotating cylinder Kozlov, Nikolai V.
 2016
 127 C p. 561-571
11 p.
 artikel
21 Effects of micro-ramp on transverse jet in supersonic crossflow Zhang, Yujie
 2016
 127 C p. 160-170
11 p.
 artikel
22 Effects of self-pulsation on the spray characteristics of gas–liquid swirl coaxial injector Kang, Zhongtao
 2016
 127 C p. 249-259
11 p.
 artikel
23 Electric sail option for cometary rendezvous Quarta, Alessandro A.
 2016
 127 C p. 684-692
9 p.
 artikel
24 ESA's billion star surveyor – Flight operations experience from Gaia's first 1.5 Years Milligan, D.
 2016
 127 C p. 394-403
10 p.
 artikel
25 Evaluation of transient response of spinning solar sail with flexible membrane by eigenfunction analysis and continuum analysis Chujo, Toshihiro
 2016
 127 C p. 542-552
11 p.
 artikel
26 Experimental investigation on combustion performance of cavity-strut injection of supercritical kerosene in supersonic model combustor Sun, Ming-bo
 2016
 127 C p. 112-119
8 p.
 artikel
27 Fast estimation of space-robots inertia parameters: A modular mathematical formulation Nabavi Chashmi, Seyed Yaser
 2016
 127 C p. 283-295
13 p.
 artikel
28 Feasibility of a low-cost sounding rockoon platform Okninski, Adam
 2016
 127 C p. 335-344
10 p.
 artikel
29 Flight status of robotic asteroid sample return mission Hayabusa2 Tsuda, Yuichi
 2016
 127 C p. 702-709
8 p.
 artikel
30 GPU-accelerated computational tool for studying the effectiveness of asteroid disruption techniques Zimmerman, Ben J.
 2016
 127 C p. 644-654
11 p.
 artikel
31 Heliocentric phasing performance of electric sail spacecraft Mengali, Giovanni
 2016
 127 C p. 474-481
8 p.
 artikel
32 IFC - Publication Information 2016
 127 C p. IFC-
1 p.
 artikel
33 Large eddy simulation of combustion characteristics in a kerosene fueled rocket-based combined-cycle engine combustor Huang, Zhi-wei
 2016
 127 C p. 326-334
9 p.
 artikel
34 Line-of-sight based formation keeping and attitude control of two spacecraft Warier, Rakesh R
 2016
 127 C p. 131-140
10 p.
 artikel
35 Midcourse trajectory correction for solar sail starships Matloff, Gregory L.
 2016
 127 C p. 699-701
3 p.
 artikel
36 Minimum-fuel station-change for geostationary satellites using low-thrust considering perturbations Zhao, ShuGe
 2016
 127 C p. 296-307
12 p.
 artikel
37 Numerical analysis of flow features and operation characteristics of a rocket-based combined-cycle inlet in ejector mode Shi, Lei
 2016
 127 C p. 182-196
15 p.
 artikel
38 Numerical exploration of mixing and combustion in a dual-mode combustor with backward-facing steps Huang, Wei
 2016
 127 C p. 572-578
7 p.
 artikel
39 Numerical investigation and optimization on mixing enhancement factors in supersonic jet-to-crossflow flow fields Yan, Li
 2016
 127 C p. 321-325
5 p.
 artikel
40 Numerical investigation of hypersonic flat-plate boundary layer transition mechanism induced by different roughness shapes Zhou, Yunlong
 2016
 127 C p. 209-218
10 p.
 artikel
41 Numerical investigation on the regression rate of hybrid rocket motor with star swirl fuel grain Zhang, Shuai
 2016
 127 C p. 384-393
10 p.
 artikel
42 On small satellites for oceanography: A survey Guerra, André G.C.
 2016
 127 C p. 404-423
20 p.
 artikel
43 On the enhanced detectability of GPS anomalous behavior with relative entropy Cho, Jeongho
 2016
 127 C p. 526-532
7 p.
 artikel
44 Parametric study of combustion oscillation in a single-side expansion scramjet combustor Ouyang, Hao
 2016
 127 C p. 603-613
11 p.
 artikel
45 Phasing Delta-V for transfers from Sun–Earth halo orbits to the Moon Chen, Hongru
 2016
 127 C p. 464-473
10 p.
 artikel
46 Polar constellations design for discontinuous coverage Sarno, Salvatore
 2016
 127 C p. 367-374
8 p.
 artikel
47 Post-launch analysis of the deployment dynamics of a space web sounding rocket experiment Mao, Huina
 2016
 127 C p. 345-358
14 p.
 artikel
48 RemoveDEBRIS: An in-orbit active debris removal demonstration mission Forshaw, Jason L.
 2016
 127 C p. 448-463
16 p.
 artikel
49 Research on the drag reduction performance induced by the counterflowing jet for waverider with variable blunt radii Li, Shi-bin
 2016
 127 C p. 120-130
11 p.
 artikel
50 Resistance forces during boulder extraction from an asteroid Kulchitsky, Anton V.
 2016
 127 C p. 424-437
14 p.
 artikel
51 Results of the attitude reconstruction for the UniSat-6 microsatellite using in-orbit data Battistini, Simone
 2016
 127 C p. 87-94
8 p.
 artikel
52 Robust, affordable, semi-direct Mars mission Salotti, Jean-Marc
 2016
 127 C p. 235-248
14 p.
 artikel
53 Robust optimal sun-pointing control of a large solar power satellite Wu, Shunan
 2016
 127 C p. 226-234
9 p.
 artikel
54 Site selection and traverse planning to support a lunar polar rover mission: A case study at Haworth Crater Heldmann, Jennifer L.
 2016
 127 C p. 308-320
13 p.
 artikel
55 Synthesis, characterization and application of ion exchange resin as a slow-release fertilizer for wheat cultivation in space Li, Bowei
 2016
 127 C p. 579-586
8 p.
 artikel
56 Test study on the performance of shielding configuration with stuffed layer under hypervelocity impact Ke, Fa-wei
 2016
 127 C p. 553-560
8 p.
 artikel
57 The evolution of Earth Observation satellites in Europe and its impact on the performance of emergency response services Denis, Gil
 2016
 127 C p. 619-633
15 p.
 artikel
58 The hybrid RANS/LES of partially premixed supersonic combustion using G/Z flamelet model Wu, Jinshui
 2016
 127 C p. 375-383
9 p.
 artikel
59 The NEOTωIST mission (Near-Earth Object Transfer of angular momentum spin test) Drube, Line
 2016
 127 C p. 103-111
9 p.
 artikel
60 Thermal behavior in the cracking reaction zone of scramjet cooling channels at different channel aspect ratios Zhang, Silong
 2016
 127 C p. 41-56
16 p.
 artikel
61 Thermal effect on the dynamic response of axially functionally graded beam subjected to a moving harmonic load Wang, Yuewu
 2016
 127 C p. 171-181
11 p.
 artikel
62 Thermal–structural analysis of the platelet heat-pipe-cooled leading edge of hypersonic vehicle Hongpeng, Liu
 2016
 127 C p. 13-19
7 p.
 artikel
63 Thrust vector control of upper stage with a gimbaled thruster during orbit transfer Wang, Zhaohui
 2016
 127 C p. 359-366
8 p.
 artikel
64 To ignite the passion in children's hearts – Role and effect of space education, issues and consideration Kojima, Ayami
 2016
 127 C p. 614-618
5 p.
 artikel
65 Toward a new spacecraft optimal design lifetime? Impact of marginal cost of durability and reduced launch price Snelgrove, Kailah B.
 2016
 127 C p. 271-282
12 p.
 artikel
66 Unscented predictive variable structure filter for satellite attitude estimation with model errors when using low precision sensors Cao, Lu
 2016
 127 C p. 505-513
9 p.
 artikel
67 Ups and downs of space tourism development in 60 years from moon register to spaceshiptwo CRASH Chang, Yi-Wei
 2016
 127 C p. 533-541
9 p.
 artikel
68 Volume magnetization for system-level testing of magnetic materials within small satellites Gerhardt, David T.
 2016
 127 C p. 1-12
12 p.
 artikel
69 When will on-orbit servicing be part of the space enterprise? Hastings, Daniel E.
 2016
 127 C p. 655-666
12 p.
 artikel
70 Yuzhnoye's new liquid rocket engines as enablers for space exploration Degtyarev, Alexander
 2016
 127 C p. 693-698
6 p.
 artikel
                             70 gevonden resultaten
 
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