Pioneer 0
Template:Short description Template:Infobox spaceflight
| Instruments | |
|---|---|
| TV camera : | Photograph the Moon |
| Magnetometer : | Interplanetary magnetic field |
| Micrometeoroid detectors : | Micrometeoroids |
Pioneer 0 (also known as Able 1) was a failed United States space probe that was designed to go into orbit around the Moon, carrying a television camera, a micrometeorite detector and a magnetometer. It was part of the first International Geophysical Year (IGY) science payload. It was designed and operated by the Air Force Ballistic Missile Division as the first spacecraft in the Pioneer program and was the first attempted launch beyond Earth orbit by any country,<ref>Template:Cite book</ref> but the rocket failed shortly after launch. The probe was intended to be called Pioneer (or Pioneer 1), but the launch failure precluded that name.
Spacecraft design
The spacecraft consisted of a thin cylindrical midsection with a squat truncated cone frustum of Template:Convert high on each side.<ref name="STL Vol. 1"/> The cylinder was Template:Convert in diameter<ref name="STL Vol. 1"/> and the height from the top of one cone to the top of the opposite cone was 76 cm. Along the axis of the spacecraft and protruding from the end of the lower cone was an Template:Convert solid propellant injection rocket and rocket case, which formed the main structural member of the spacecraft. Eight small low-thrust solid propellant velocity adjustment rockets were mounted on the end of the upper cone in a ring assembly which could be jettisoned after use. A magnetic dipole antenna also protruded from the top of the upper cone. The shell was composed of laminated plastic and was painted with a pattern of dark and light stripes to help regulate temperature.
The scientific instrument package had a mass of Template:Convert and consisted of:
- An image scanning infrared television system of the Naval Ordnance Test Station (NOTS) design to study the Moon's surface, particularly the part normally unseen from Earth.<ref name="STL Vol. 2"/>
- A diaphragm/microphone assembly to detect micrometeorites. A micrometeorite hitting the diaphragm would generate an acoustic pulse that would travel through the diaphragm to the microphone. The microphone contained a piezoelectrical crystal that rang at 100 kc under influence of the acoustic pulse. A bandpass amplifier would amplify the signal, so it could be detected.<ref name="STL Vol. 2"/>
- A search-coil magnetometer with nonlinear amplifier to measure the Earth's, Moon's and interplanetary magnetic field. At the time, it was not known whether the Moon had a magnetic field or not.<ref name="STL Vol. 2"/>
The spacecraft was powered by nickel-cadmium batteries for ignition of the rockets, silver cell batteries for the television system, and mercury batteries for the remaining circuits. Radio transmission was on 108.06 MHz, a standard frequency used by satellites in the International Geophysical Year,<ref name="Quest Feb14"> Template:Cite news</ref> through an electric dipole antenna for telemetry and doppler information and a magnetic dipole antenna for the television system. Ground commands were received through the electric dipole antenna at 115 MHz. The spacecraft was to be spin-stabilized at 1.8 revolutions per second, the spin direction approximately perpendicular to the geomagnetic meridian planes of the trajectory.
Launch and failure
Pioneer 0 was launched on Thor missile number 127 at 12:18:00 GMT on 17 August 1958 by the Air Force Ballistic Missile Division, only 4 minutes after the scheduled launch time.<ref name="STL Vol. 1"/> It was destroyed by an explosion of the first stage of the Thor booster, 73.6 seconds after lift-off<ref name="STL Vol. 1"/> at Template:Convert altitude, Template:Convert downrange over the Atlantic Ocean. The failure was suspected to be due to a turbopump bearing that came loose, causing the liquid oxygen pump to stop. The abrupt loss of thrust caused the Thor to lose attitude control and pitch downward, which caused the LOX tank to rupture from aerodynamic loads and resulting in complete destruction of the launch vehicle.<ref name="STL Vol. 1"/> Erratic telemetry signals were received from the payload and upper stages for 123 seconds after the explosion, and the upper stages were tracked to impact in the ocean. The original plan was for the spacecraft to travel for 2.6 days to the Moon, at which time a TX-8-6 solid-propellant motor would fire to put it into a Template:Convert lunar orbit which was to nominally last for about two weeks. Air Force officials stated that they were not surprised at the failure, adding that "it would have been more of a shock had the mission succeeded."Template:Citation needed It was the only mission in the Project Able-1 Probes (USAF) entirely run by the Air Force Ballistic Missile Division, as subsequent missions were conducted by NASA.<ref name="Quicklook"/>
References
External links
- United States Space Program Progress 1958 discusses Pioneer 0 - 3 at YouTube
- Pioneers 0-2 documents at Space Technology Laboratories archive