Pioneer P-1: Difference between revisions
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| manufacturer = {{flagicon|USA}} [[TRW Inc.|Space Technology |
| manufacturer = {{flagicon|USA}} [[TRW Inc.|Space Technology Laboratories]] |
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| dry_mass = {{convert|25.3|kg|lb}} |
| dry_mass = {{convert|25.3|kg|lb}} |
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| launch_mass = {{convert|88.4|kg|lb}} |
| launch_mass = {{convert|88.4|kg|lb}} |
Revision as of 22:53, 4 January 2020
Mission type | Lunar flyby |
---|---|
Operator | NASA |
COSPAR ID | 1959-E02 |
Mission duration | Failure to launch |
Spacecraft properties | |
Manufacturer | Space Technology Laboratories |
Launch mass | 88.4 kilograms (195 lb) |
Dry mass | 25.3 kilograms (56 lb) |
Start of mission | |
Launch date | September 24, 1959, 05:44:52 | UTC
Rocket | Atlas C Able |
Launch site | Cape Canaveral LC-12 |
Pioneer P-1 was a failed mission in the Pioneer program. The spacecraft was a 1-meter diameter sphere, with a propulsion module. It was launched on 24 September 1959 on an Atlas C-Able launcher. It was to carry a TV camera and a magnetic field sensor. It was to be spin-stabilized and was known as a 'paddlewheel' spacecraft. The Atlas-Able launch vehicle was destroyed in an explosion on the launch pad at Cape Canaveral during a pre-launch static firing. The payload of P-1 spacecraft and Able IV space engine was not present on the launch vehicle when it exploded, and the payload was later used in the P-3 mission.[1][2]
References
- ^ Gunter's Space Page - information on Pioneer P-1
- ^ New York Times, "U.S. Moon Rocket Blows Up in Test", Sept 25, 1959