Editing Pioneer P-3 (section)

== Spacecraft design ==
[[File:Able IV World's First Space Engine.jpg|thumb|Propulsion system of Pioneer P-3]]
Pioneer P-3 was a 1-meter diameter sphere with a [[monopropellant]] propulsion system mounted on the bottom giving a total length of 1.4 meters. The mass of the structure and aluminum alloy shell was 25.3&nbsp;kg and the propulsion units 88.4&nbsp;kg. Four solar panels, each 60 x 60&nbsp;cm and containing 2200 solar cells in 22 100-cell nodules, extended from the sides of the spherical shell in a "paddle-wheel" configuration with a total span of about 2.7 meters. The solar panels charged chemical 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. This space engine was designed and built under contract with NASA by the Space Technology Laboratories (STL) of [[TRW Inc.|TRW]].<ref name="able4b">{{cite web |title=Able 4B (Pioneer P-3) |url=https://science.nasa.gov/mission/pioneer-p-3-able-4b/ |website=NASA |access-date=May 18, 2025}}</ref>

Around the upper hemisphere of the hydrazine tank was a ring-shaped instrument platform which held the batteries in two packs, two 5 W [[UHF]] transmitters and [[diplexer]]s, 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.<ref name="exmachina">{{cite web|title=You Can’t Fail Unless You Try: NASA’s Pioneer P-3 Lunar Orbiter |first=Andrew |last=LePage |url=https://www.drewexmachina.com/2024/11/26/you-cant-fail-unless-you-try-nasas-pioneer-p-3-lunar-orbiter/ |date=November 26, 2024 |access-date=May 18, 2025}}</ref>

Thermal control was planned to be achieved by a large number of small "propeller blade" devices on the surface of the sphere. The blades themselves were made of reflective material and consist of four vanes that 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.<ref name="exmachina"/>