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 |