| 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
|
52 |
2-6 |
p. 371-379
9 p.
|
artikel
|
| 2 |
Advanced ion propulsion systems for affordable deep-space missions
|
Brophy, John
|
|
2003
|
52 |
2-6 |
p. 309-316
8 p.
|
artikel
|
| 3 |
Advanced system on a chip microelectronics for spacecraft and science instruments
|
Paschalidis, Nikolaos P.
|
|
2003
|
52 |
2-6 |
p. 411-420
10 p.
|
artikel
|
| 4 |
Advances in deep-space telecommunications technology at the Applied Physics Laboratory
|
Bokulic, R.S
|
|
2003
|
52 |
2-6 |
p. 467-474
8 p.
|
artikel
|
| 5 |
AIMS: Acousto-optic imaging spectrometer for spectral mapping of solid surfaces
|
Glenar, David A.
|
|
2003
|
52 |
2-6 |
p. 389-396
8 p.
|
artikel
|
| 6 |
Aladdin mission concept
|
Mueller, J.T.
|
|
2003
|
52 |
2-6 |
p. 211-218
8 p.
|
artikel
|
| 7 |
An autonomous navigation and guidance system for MUSES-C asteroid landing
|
Kubota, Takashi
|
|
2003
|
52 |
2-6 |
p. 125-131
7 p.
|
artikel
|
| 8 |
A new compression algorithm for spectral and time-series data
|
Hawkins III, S.Edward
|
|
2003
|
52 |
2-6 |
p. 487-492
6 p.
|
artikel
|
| 9 |
Applying successful near mission operations approaches and refining for contour mission operations
|
Holdridge, Mark E.
|
|
2003
|
52 |
2-6 |
p. 343-352
10 p.
|
artikel
|
| 10 |
A solar powered spacecraft for the INSIDE Jupiter mission
|
Jonaitis, John
|
|
2003
|
52 |
2-6 |
p. 237-244
8 p.
|
artikel
|
| 11 |
Attitude determination and control system design of the ITU-UUBF LEO1 satellite
|
Hajiyev, Ch.
|
|
2003
|
52 |
2-6 |
p. 493-499
7 p.
|
artikel
|
| 12 |
Deep Impact: mission design approach for a new Discovery mission
|
Blume, William H
|
|
2003
|
52 |
2-6 |
p. 105-110
6 p.
|
artikel
|
| 13 |
Development of micro-manipulator for tele-science by lunar rover: Micro5
|
Kunii, Yasuharu
|
|
2003
|
52 |
2-6 |
p. 433-439
7 p.
|
artikel
|
| 14 |
Europa Lander
|
Gershman, Robert
|
|
2003
|
52 |
2-6 |
p. 253-258
6 p.
|
artikel
|
| 15 |
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
|
52 |
2-6 |
p. 327-335
9 p.
|
artikel
|
| 16 |
Launch vehicles for low-cost planetary missions
|
Palsulich, Joseph M.
|
|
2003
|
52 |
2-6 |
p. 289-298
10 p.
|
artikel
|
| 17 |
Light weight sensors for the autonomous asteroid landing of MUSES-C mission
|
Hashimoto, Tatsuaki
|
|
2003
|
52 |
2-6 |
p. 381-388
8 p.
|
artikel
|
| 18 |
Low cost access to Mars—Mars micromissions spacecraft
|
Deininger, W.D
|
|
2003
|
52 |
2-6 |
p. 501-510
10 p.
|
artikel
|
| 19 |
Low-cost interstellar probe
|
McNutt Jr., R.L.
|
|
2003
|
52 |
2-6 |
p. 267-279
13 p.
|
artikel
|
| 20 |
LUGH/Mercury express: a proposed multi-platform flyby mission to Mercury
|
Clark, P.E.
|
|
2003
|
52 |
2-6 |
p. 181-188
8 p.
|
artikel
|
| 21 |
Mainbelt asteroid reconnaisance and sample return using solar electric propulsion
|
Wolf, Aron A
|
|
2003
|
52 |
2-6 |
p. 133-141
9 p.
|
artikel
|
| 22 |
Mars Express—ESA's first mission to planet Mars
|
Schmidt, R.
|
|
2003
|
52 |
2-6 |
p. 197-202
6 p.
|
artikel
|
| 23 |
Mars Express spacecraft: design and development solutions for affordable planetary missions
|
Moulinier, P.
|
|
2003
|
52 |
2-6 |
p. 203-209
7 p.
|
artikel
|
| 24 |
Mars network for enabling low-cost missions
|
Hastrup, R.C.
|
|
2003
|
52 |
2-6 |
p. 227-235
9 p.
|
artikel
|
| 25 |
MArs Neutron Energy Spectrometer (MANES): an instrument for the Mars 2003 Lander
|
Maurer, Richard H.
|
|
2003
|
52 |
2-6 |
p. 405-410
6 p.
|
artikel
|
| 26 |
Micro-hopping robot for asteroid exploration
|
Yoshimitsu, Tetsuo
|
|
2003
|
52 |
2-6 |
p. 441-446
6 p.
|
artikel
|
| 27 |
Micromachined polysilicon resonating xylophone bar magnetometer
|
Wickenden, D.K.
|
|
2003
|
52 |
2-6 |
p. 421-425
5 p.
|
artikel
|
| 28 |
Miniature time-of-flight mass spectrometers for in situ composition studies
|
Brinckerhoff, W.B.
|
|
2003
|
52 |
2-6 |
p. 397-404
8 p.
|
artikel
|
| 29 |
On the comet rendezvous exploration and its potential extension via solar electric propulsion (Comet Nucleus Sample and Return Mission)
|
Kawaguchi, Jun'ichiro
|
|
2003
|
52 |
2-6 |
p. 143-149
7 p.
|
artikel
|
| 30 |
Overcoming Genesis mission design challenges
|
Williams, Kenneth E.
|
|
2003
|
52 |
2-6 |
p. 281-287
7 p.
|
artikel
|
| 31 |
Predicting mission success in small satellite missions
|
Saunders, Mark
|
|
2003
|
52 |
2-6 |
p. 361-370
10 p.
|
artikel
|
| 32 |
Preface
|
Farquhar, Robert
|
|
2003
|
52 |
2-6 |
p. 77-
1 p.
|
artikel
|
| 33 |
Saturn Ring Observer
|
Spilker, Thomas R.
|
|
2003
|
52 |
2-6 |
p. 259-265
7 p.
|
artikel
|
| 34 |
Scientific objectives of the Beagle 2 lander
|
Wright, I.P.
|
|
2003
|
52 |
2-6 |
p. 219-225
7 p.
|
artikel
|
| 35 |
Selected configuration tradeoffs of contour optical instruments
|
Warren, J.
|
|
2003
|
52 |
2-6 |
p. 111-116
6 p.
|
artikel
|
| 36 |
Small, light-weight rover “Micro5” for lunar exploration
|
Kubota, Takashi
|
|
2003
|
52 |
2-6 |
p. 447-453
7 p.
|
artikel
|
| 37 |
SMART-1: key technologies and autonomy implementations
|
Elfving, A.
|
|
2003
|
52 |
2-6 |
p. 475-486
12 p.
|
artikel
|
| 38 |
Solar sail technology development and demonstration
|
Leipold, M
|
|
2003
|
52 |
2-6 |
p. 317-326
10 p.
|
artikel
|
| 39 |
Space technology three: mission overview and spacecraft concept description
|
Deininger, W.D.
|
|
2003
|
52 |
2-6 |
p. 455-465
11 p.
|
artikel
|
| 40 |
STARDUST: implementing a new manage-to-budget paradigm
|
Atkins, Kenneth L
|
|
2003
|
52 |
2-6 |
p. 87-97
11 p.
|
artikel
|
| 41 |
Synthesis of an alternative flight trajectory for Mars explorer, Nozomi
|
Kawaguchi, Jun'ichiro
|
|
2003
|
52 |
2-6 |
p. 189-195
7 p.
|
artikel
|
| 42 |
The CONTOUR mission—status of implementation
|
Chiu, M.C.
|
|
2003
|
52 |
2-6 |
p. 99-103
5 p.
|
artikel
|
| 43 |
The CONTOUR remote imager and spectrograph
|
Fort, D.
|
|
2003
|
52 |
2-6 |
p. 427-431
5 p.
|
artikel
|
| 44 |
The ESA approach to low-cost planetary missions
|
Whitcomb, G.P
|
|
2003
|
52 |
2-6 |
p. 79-86
8 p.
|
artikel
|
| 45 |
The MUSES-C mission for the sample and return—its technology development status and readiness
|
Kawaguchi, Jun'ichiro
|
|
2003
|
52 |
2-6 |
p. 117-123
7 p.
|
artikel
|
| 46 |
The Rockot launch system—the commercial solution for low-cost planetary missions
|
Freeborn, P
|
|
2003
|
52 |
2-6 |
p. 299-307
9 p.
|
artikel
|
| 47 |
Transfers to Earth centered orbits via lunar gravity assist
|
Ocampo, Cesar A.
|
|
2003
|
52 |
2-6 |
p. 173-179
7 p.
|
artikel
|
| 48 |
Trends in cost-effective mission operations
|
van der Ha, Jozef
|
|
2003
|
52 |
2-6 |
p. 337-342
6 p.
|
artikel
|
| 49 |
Utilising Rosetta commonality to reduce mission operations cost for Mars Express
|
Ferri, Paolo
|
|
2003
|
52 |
2-6 |
p. 353-359
7 p.
|
artikel
|
| 50 |
Venus sample return missions—a range of science, a range of costs
|
Sweetser, Ted
|
|
2003
|
52 |
2-6 |
p. 165-172
8 p.
|
artikel
|
| 51 |
Venus stratospheric sounder: first in situ measurements in upper cloud region
|
Kerzhanovich, Viktor V.
|
|
2003
|
52 |
2-6 |
p. 159-164
6 p.
|
artikel
|
| 52 |
VEVA Discovery mission to Venus: exploration of volcanoes and atmosphere
|
Klaasen, Kenneth P.
|
|
2003
|
52 |
2-6 |
p. 151-158
8 p.
|
artikel
|
| 53 |
VOLCAN: a mission to explore Jupiter's volcanic moon Io
|
Esper, Jaime
|
|
2003
|
52 |
2-6 |
p. 245-251
7 p.
|
artikel
|
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