Editing Pioneer P-30 (section)

== Spacecraft design ==

Pioneer P-30 was almost identical to the earlier [[Pioneer P-3]] satellite which failed, a 1-meter diameter sphere with a propulsion system mounted on the bottom giving a total length of {{convert|1.4|m|in|sp=us}}. The mass of the structure and aluminum alloy shell was about {{cvt|30|kg|lb}} and the propulsion units roughly {{cvt|90|kg}}. Four [[solar panel]]s, each {{cvt|60|x|60|cm|in}} and containing 2200 [[solar cell]]s in 22 100-cell nodules, extended from the sides of the spherical shell in a "paddle-wheel" configuration with a total span of about {{convert|2.7|m|in|sp=us}}. The solar panels charged [[nickel-cadmium battery|nickel-cadmium batteries]]. Inside the shell, a large spherical hydrazine tank made up most of the volume, topped by two smaller spherical nitrogen tanks and a 90 N injection rocket to slow the spacecraft down to go into lunar orbit, which was designed to be capable of firing twice during the mission. Attached to the bottom of the sphere was a 90 N vernier rocket for mid-course propulsion and lunar orbit maneuvers which could be fired four times.

Around the upper hemisphere of the hydrazine tank was a ring-shaped instrument platform which held the batteries in two packs, two 1.5 W UHF transmitters and diplexers, logic modules for scientific instruments, two command receivers, decoders, a buffer/amplifier, three converters, a telebit, a command box, and most of the scientific instruments. Two dipole UHF antennas protruded from the top of the sphere on either side of the injection rocket nozzle. Two dipole UHF antennas and a long VLF antenna protruded from the bottom of the sphere. The transmitters operated on a frequency of 378 [[megahertz]].

Thermal control was planned to be achieved by fifty small "propeller blade" devices on the surface of the sphere. The blades themselves were made of reflective material and consist of four vanes which were flush against the surface, covering a black heat-absorbing pattern painted on the sphere. A thermally sensitive coil was attached to the blades in such a way that low temperatures within the satellite would cause the coil to contract and rotate the blades and expose the heat-absorbing surface, and high temperatures would cause the blades to cover the black patterns. Square heat-sink units were also mounted on the surface of the sphere to help dissipate heat from the interior.