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                             102 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 A complexity-based risk assessment of low-cost planetary missions: when is a mission too fast and too cheap? Bearden, David A.
2003
2-6 p. 371-379
9 p.
artikel
2 Advanced ion propulsion systems for affordable deep-space missions Brophy, John
2003
2-6 p. 309-316
8 p.
artikel
3 Advanced microelectronics technologies for future small satellite systems Alkalai, Leon
2000
2-6 p. 233-239
7 p.
artikel
4 Advanced system on a chip microelectronics for spacecraft and science instruments Paschalidis, Nikolaos P.
2003
2-6 p. 411-420
10 p.
artikel
5 Advances in deep-space telecommunications technology at the Applied Physics Laboratory Bokulic, R.S
2003
2-6 p. 467-474
8 p.
artikel
6 AIMS: Acousto-optic imaging spectrometer for spectral mapping of solid surfaces Glenar, David A.
2003
2-6 p. 389-396
8 p.
artikel
7 Aladdin mission concept Mueller, J.T.
2003
2-6 p. 211-218
8 p.
artikel
8 A low-power high-speed smart sensor design for space exploration missions Fang, Wai-Chi
2000
2-6 p. 241-250
10 p.
artikel
9 AMORE: An autonomous constellation concept for atmospheric and ocean observation Yunck, T.P.
2000
2-6 p. 355-364
10 p.
artikel
10 An autonomous navigation and guidance system for MUSES-C asteroid landing Kubota, Takashi
2003
2-6 p. 125-131
7 p.
artikel
11 An Earth observation mission based on the MiniSIL™ platform Ward, A.K.
2000
2-6 p. 87-96
10 p.
artikel
12 A new compression algorithm for spectral and time-series data Hawkins III, S.Edward
2003
2-6 p. 487-492
6 p.
artikel
13 An experimental low-cost ground station for the small satellite project BIRD Kayal, Hakan
2000
2-6 p. 213-220
8 p.
artikel
14 Application of industrial CAN bus technology for LEO-satellites Janschek, Klaus
2000
2-6 p. 313-317
5 p.
artikel
15 Application of micro-mechanic devices for motion compensation of space-borne CCD-imaging systems Walter, Ingo
2000
2-6 p. 269-277
9 p.
artikel
16 Applying successful near mission operations approaches and refining for contour mission operations Holdridge, Mark E.
2003
2-6 p. 343-352
10 p.
artikel
17 ASAP 5—Low-cost access to space for auxiliary payloads Balaam, Philip
2000
2-6 p. 127-133
7 p.
artikel
18 A solar powered spacecraft for the INSIDE Jupiter mission Jonaitis, John
2003
2-6 p. 237-244
8 p.
artikel
19 A technology path to distributed remote sensing Fountain, Glen H.
2000
2-6 p. 251-261
11 p.
artikel
20 Attitude control system for the first swedish nanosatellite “MUNIN” Ovchinnikov, Michael
2000
2-6 p. 319-326
8 p.
artikel
21 Attitude determination and control system design of the ITU-UUBF LEO1 satellite Hajiyev, Ch.
2003
2-6 p. 493-499
7 p.
artikel
22 CESAR Mission—Cooperation Española-Argentina Acedo, Lucía
2000
2-6 p. 121-126
6 p.
artikel
23 CHAMP attitude and orbit control system Schmitt, Christian
2000
2-6 p. 327-333
7 p.
artikel
24 CNES small satellites Earth observation scientific future missions Blouvac, Jean
2000
2-6 p. 75-79
5 p.
artikel
25 Compact High Resolution Imaging Spectrometer (CHRIS) Cutter, Mike A
2000
2-6 p. 263-268
6 p.
artikel
26 CONAE's satellite missions Caruso, Daniel
2000
2-6 p. 389-395
7 p.
artikel
27 Data reception of small satellites in a multimission scenario Schwarz, Joachim
2000
2-6 p. 221-228
8 p.
artikel
28 Deep Impact: mission design approach for a new Discovery mission Blume, William H
2003
2-6 p. 105-110
6 p.
artikel
29 Design of SmArT microsatellite deployable solar wings Fragnito, Marino
2000
2-6 p. 335-344
10 p.
artikel
30 Development of micro-manipulator for tele-science by lunar rover: Micro5 Kunii, Yasuharu
2003
2-6 p. 433-439
7 p.
artikel
31 Earth observation program with small satellites at OHB-system Ginati, Amnon
2000
2-6 p. 297-306
10 p.
artikel
32 Europa Lander Gershman, Robert
2003
2-6 p. 253-258
6 p.
artikel
33 Feasibility demonstration of a high performance compact telescope Laubier, D.
2000
2-6 p. 279-286
8 p.
artikel
34 Flight dynamics lessons of INTERBALL project Eismont, Nathan A.
2000
2-6 p. 405-414
10 p.
artikel
35 Impact of the “faster better cheaper” requirements for satellites components/subsystems on SEP organistion and processes Pages, X.
2000
2-6 p. 179-185
7 p.
artikel
36 Johns Hopkins APL paradigm in smallsat management Krimigis, S.M.
2000
2-6 p. 187-197
11 p.
artikel
37 Launch configurations based on former (now decommissioned) Soviet ICBMs and Soyuz–Fregat, coupled with plasma propulsion as delivery systems for low cost missions beyond low earth orbits Karavasilis, K
2003
2-6 p. 327-335
9 p.
artikel
38 Launch vehicles for low-cost planetary missions Palsulich, Joseph M.
2003
2-6 p. 289-298
10 p.
artikel
39 Light weight sensors for the autonomous asteroid landing of MUSES-C mission Hashimoto, Tatsuaki
2003
2-6 p. 381-388
8 p.
artikel
40 Low cost access to Mars—Mars micromissions spacecraft Deininger, W.D
2003
2-6 p. 501-510
10 p.
artikel
41 Low-cost interstellar probe McNutt Jr., R.L.
2003
2-6 p. 267-279
13 p.
artikel
42 LUGH/Mercury express: a proposed multi-platform flyby mission to Mercury Clark, P.E.
2003
2-6 p. 181-188
8 p.
artikel
43 Mainbelt asteroid reconnaisance and sample return using solar electric propulsion Wolf, Aron A
2003
2-6 p. 133-141
9 p.
artikel
44 Mars Express—ESA's first mission to planet Mars Schmidt, R.
2003
2-6 p. 197-202
6 p.
artikel
45 Mars Express spacecraft: design and development solutions for affordable planetary missions Moulinier, P.
2003
2-6 p. 203-209
7 p.
artikel
46 Mars network for enabling low-cost missions Hastrup, R.C.
2003
2-6 p. 227-235
9 p.
artikel
47 MArs Neutron Energy Spectrometer (MANES): an instrument for the Mars 2003 Lander Maurer, Richard H.
2003
2-6 p. 405-410
6 p.
artikel
48 Micro-hopping robot for asteroid exploration Yoshimitsu, Tetsuo
2003
2-6 p. 441-446
6 p.
artikel
49 Micromachined polysilicon resonating xylophone bar magnetometer Wickenden, D.K.
2003
2-6 p. 421-425
5 p.
artikel
50 MIMOSA satellite Peresty, R.
2000
2-6 p. 345-349
5 p.
artikel
51 Miniature time-of-flight mass spectrometers for in situ composition studies Brinckerhoff, W.B.
2003
2-6 p. 397-404
8 p.
artikel
52 NASA-GSFC nano-satellite technology for Earth science missions Esper, Jaime
2000
2-6 p. 287-296
10 p.
artikel
53 NASA's Earth science program—increasing science opportunity and payoff through small satellites Paules, Granville
2000
2-6 p. 61-64
4 p.
artikel
54 NASA's X2000 program—An institutional approach to enabling smaller spacecraft Deutsch, Leslie J.
2000
2-6 p. 229-232
4 p.
artikel
55 New Micro Satellite concept for observation missions Kawada, Y.
2000
2-6 p. 159-167
9 p.
artikel
56 On the comet rendezvous exploration and its potential extension via solar electric propulsion (Comet Nucleus Sample and Return Mission) Kawaguchi, Jun'ichiro
2003
2-6 p. 143-149
7 p.
artikel
57 Orbital launch systems Pao, Cary D.
2000
2-6 p. 145-153
9 p.
artikel
58 Overcoming Genesis mission design challenges Williams, Kenneth E.
2003
2-6 p. 281-287
7 p.
artikel
59 Predicting mission success in small satellite missions Saunders, Mark
2003
2-6 p. 361-370
10 p.
artikel
60 Preface Farquhar, Robert
2003
2-6 p. 77-
1 p.
artikel
61 Preface 2000
2-6 p. xi-xii
nvt p.
artikel
62 PRIMA: A new, competitive small satellite platform Galeazzi, Claudio
2000
2-6 p. 379-388
10 p.
artikel
63 Radiation impacts on star-tracker performance and vision systems in space Jørgensen, John L.
2000
2-6 p. 415-422
8 p.
artikel
64 RapidEye satellite based geo-information system Krischke, M.
2000
2-6 p. 307-312
6 p.
artikel
65 ROCKOT: The proven, competitive launch system for small satellites Freeborn, P.
2000
2-6 p. 135-143
9 p.
artikel
66 Saturn Ring Observer Spilker, Thomas R.
2003
2-6 p. 259-265
7 p.
artikel
67 Scientific objectives of the Beagle 2 lander Wright, I.P.
2003
2-6 p. 219-225
7 p.
artikel
68 Selected configuration tradeoffs of contour optical instruments Warren, J.
2003
2-6 p. 111-116
6 p.
artikel
69 Small, light-weight rover “Micro5” for lunar exploration Kubota, Takashi
2003
2-6 p. 447-453
7 p.
artikel
70 Small satellites: Enabling operational disaster management systems Tobias, Alberto
2000
2-6 p. 101-109
9 p.
artikel
71 Small satellites for Earth observation — The German small satellite programme Liebig, Volker
2000
2-6 p. 81-86
6 p.
artikel
72 SMART-1: key technologies and autonomy implementations Elfving, A.
2003
2-6 p. 475-486
12 p.
artikel
73 Solar sail technology development and demonstration Leipold, M
2003
2-6 p. 317-326
10 p.
artikel
74 Space technology three: mission overview and spacecraft concept description Deininger, W.D.
2003
2-6 p. 455-465
11 p.
artikel
75 STARDUST: implementing a new manage-to-budget paradigm Atkins, Kenneth L
2003
2-6 p. 87-97
11 p.
artikel
76 STARSEM—A reliable and affordable space transportation system Luciani, Bernard
2000
2-6 p. 155-157
3 p.
artikel
77 Summary of the Small Satellites for Earth Observation 2nd International Symposium of the International Academy of Astronautics Berlin, Germany April 12–16, 1999 Fountain, G.H.
2000
2-6 p. 433-440
8 p.
artikel
78 Synthesis of an alternative flight trajectory for Mars explorer, Nozomi Kawaguchi, Jun'ichiro
2003
2-6 p. 189-195
7 p.
artikel
79 The CONTOUR mission—status of implementation Chiu, M.C.
2003
2-6 p. 99-103
5 p.
artikel
80 The CONTOUR remote imager and spectrograph Fort, D.
2003
2-6 p. 427-431
5 p.
artikel
81 The Danish small satellite programme is a reality! Thomsen, Per Lundahl
2000
2-6 p. 97-100
4 p.
artikel
82 The determination of the attitude and attitude dynamics of TeamSat Betto, Maurizio
2000
2-6 p. 423-432
10 p.
artikel
83 The DLR small satellite mission BIRD Brieβ, K.
2000
2-6 p. 111-120
10 p.
artikel
84 The ESA approach to low-cost planetary missions Whitcomb, G.P
2003
2-6 p. 79-86
8 p.
artikel
85 The evolution of ESA's Earth Explorer missions Tobias, Alberto
2000
2-6 p. 65-74
10 p.
artikel
86 The future ESA Earth-Observation strategy and ESA's ‘Living Planet’ programme Southwood, D.J.
2000
2-6 p. 55-60
6 p.
artikel
87 The general conception of the microsatellite compass to be launched from submarine to study of the earthquakes forerunners Dokukin, V.S.
2000
2-6 p. 351-354
4 p.
artikel
88 The Israeli microsatellite TECHSAT for scientific and technological research: Development and in-orbit testing Guelman, M.
2000
2-6 p. 397-404
8 p.
artikel
89 The K-1 reusable aerospace vehicle: managing to achieve low cost Mueller (HM), George E.
2000
2-6 p. 199-202
4 p.
artikel
90 The LEOSTAR™ solution for high performance Earth observation missions Durteste, Christophe
2000
2-6 p. 169-177
9 p.
artikel
91 The MUSES-C mission for the sample and return—its technology development status and readiness Kawaguchi, Jun'ichiro
2003
2-6 p. 117-123
7 p.
artikel
92 The Rockot launch system—the commercial solution for low-cost planetary missions Freeborn, P
2003
2-6 p. 299-307
9 p.
artikel
93 The use of small satellites in the NASA Earth Science Enterprise (ESE) Earth Observing System (EOS) Paxton, Larry J.
2000
2-6 p. 365-374
10 p.
artikel
94 Transfers to Earth centered orbits via lunar gravity assist Ocampo, Cesar A.
2003
2-6 p. 173-179
7 p.
artikel
95 Trends in cost-effective mission operations van der Ha, Jozef
2003
2-6 p. 337-342
6 p.
artikel
96 Turkish small satellite program: Goals and policies Aşkar, Murat
2000
2-6 p. 375-378
4 p.
artikel
97 Using forward error correction technique for microsatellite data broadcasting system Hsiao, Fei-Bin
2000
2-6 p. 203-211
9 p.
artikel
98 Utilising Rosetta commonality to reduce mission operations cost for Mars Express Ferri, Paolo
2003
2-6 p. 353-359
7 p.
artikel
99 Venus sample return missions—a range of science, a range of costs Sweetser, Ted
2003
2-6 p. 165-172
8 p.
artikel
100 Venus stratospheric sounder: first in situ measurements in upper cloud region Kerzhanovich, Viktor V.
2003
2-6 p. 159-164
6 p.
artikel
101 VEVA Discovery mission to Venus: exploration of volcanoes and atmosphere Klaasen, Kenneth P.
2003
2-6 p. 151-158
8 p.
artikel
102 VOLCAN: a mission to explore Jupiter's volcanic moon Io Esper, Jaime
2003
2-6 p. 245-251
7 p.
artikel
                             102 gevonden resultaten
 
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