9 Concluding Comments
This paper discussed the principles of operation and status of spacecraft Doppler tracking, the
current-generation GW detector technology in the

10
–6 to 10
–1 Hz band. Doppler tracking differs from
all other currently-operating detectors in that the size of the apparatus (earth-spacecraft distance) is large
compared with the GW wavelength. As a consequence times-of-flight of GWs and radio waves through the
apparatus are important, resulting in a three-pulse signal response and various two-pulse noise responses.
The different signal and noise transfer functions suggest data analysis approaches for various waveforms;
some of these approaches were outlined here. The sensitivity of current-generation Doppler observations was
discussed as well as what would be required to improve this sensitivity by another order of magnitude (to

10
–17 for sinusoidal waves). Further large sensitivity improvements in the low-frequency band
will require dedicated multi-spacecraft arrays in space. Until such a dedicated mission flys,
spacecraft tracking will provide the best observational capability in the low-frequency GW
band.