The Johns Hopkins University Applied Physics Laboratory (JHU/APL) was respo
nsible for the design and fabrication of the ACE spacecraft to accommodate
the ACE Mission requirements and for the integration, test, and launch supp
ort for the entire ACE Observatory. The primary ACE Mission includes a sign
ificant number of science instruments - nine - whose diverse requirements h
ad to be factored into the overall spacecraft bus design. Secondary mission
s for monitoring space weather and measuring launch vibration environments
were also accommodated within the spacecraft design. Substantial coordinati
on and cooperation were required between the spacecraft and instrument engi
neers, and all requirements were met. Overall, the spacecraft was kept as s
imple as possible in meeting requirements to achieve a highly reliable and
low-cost design.