REBELSAT-1

OVERVIEW

SIZE

CUBESAT (3U)

ORBIT

LOW EARTH ORBIT (LEO)

INCLINATION

51.6°

ALTITUDE

350 km / 218 mi

MASS

6 kg / 13.2 lb

TYPE

SCIENTIFIC PAYLOAD

LIFETIME

1 YEAR

WHERE WE'RE AT:

The NASA Systems Engineering Handbook defines PDR as the timeline milestone which "demonstrates that preliminary design meets all system requirements with acceptable risk and within cost & schedule restraints". The RebelSat-1 team will show that correct design options have been selected with all interfaces identified. Completion of PDR entails and established basis for proceeding with the final design.

PRELIMINARY DESIGN REVIEW (PDR)

For information about any other technical details, contact rebelsat@unlv.edu