The TD-1 (Thor Delta) satellite - named after the launch vehicle - carried seven
experiments devoted to astophysical studies. Its scientific mission was to make a
systematic sky survey in the ultraviolet and high-energy regions of the spectrum. The
experiments were divided into two main categories: five experiments--measuring
ultraviolet, x and gamma rays, and heavy nuclei--scanned strips of the sky; the other two
viewed along the sun-pointing x axis and measured solar x and gamma rays.
The satellite was a triaxially stabilized platform with the × axis always pointed at
the center of the sun with an accuracy of 1 arc min. The satellite rotated around this
axis at a constant rate of 1 revolution per orbit during normal operations when sun
sensors were used for stabilization but it was spun up during eclipse periods to maintain
attitude. The sky-scanning instruments were able to scan a narrow band of the sky during
each orbit and the whole celestial sphere in 6 months. Two and one-half complete scans of
the celestial sphere were completed before the attitude control was lost in May 1974
following exhaustion of the on-board gas supply.
Despite intermittent tape recorder failure, data coverage was achieved over 95 percent
of the celestial sphere and many areas were observed during two or three separate scans.
The spacecraft was a rectangular structure and comprised a bottom compartment containing
the spacecraft subsystems and a top compartment containing the outward-viewing science
instruments. It had a cross section of 1 by 0.9 m and was 2.2 m high; its mass was 473 kg
including 120 kg of instruments.