Small-satellite technology and applications III
14-15 April 1993, Orlando, Florida Brian J. Horais, Society of Photo-optical Instrumentation Engineers ... is a , spin-stabilized, inertially oriented satellite that is weight and volume compatible with the Taurus and Pegasus launch vehicles. ... Other key characteristics of the spacecraft are shown in Figure 4-2 and a functional block diagram of the satellite is shown in Figure 4-3. ... In addition, by fabricating a second wire harness, we have produced a fully-functional satellite breadboard.
| Title | : | Small-satellite technology and applications III |
| Author | : | Brian J. Horais, Society of Photo-optical Instrumentation Engineers |
| Publisher | : | - 1993 |
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