Goals: Mariner 1 was the first attempt by the United States to send a spacecraft to Venus. It was to fly by the planet at a distance of about 29,000 km (about 18,000 miles), transmitting a variety of scientific data but no pictures.
Accomplishments: None. A problem with the guidance system shortly after launch made steering impossible and directed the spacecraft toward a crash, possibly in North Atlantic shipping lanes or in an inhabited area. The Range Safety Officer issued a destruct command about 5 minutes after launch, just 6 seconds before the spacecraft would have separated from its booster, after which the launch vehicle could not have been destroyed.
22 Jul 1962: Launch
Mission Type: Flyby
Launch Vehicle: Atlas-Agena B (no. 5 / Atlas D no. 145 / Agena B no. 6901)
Launch Site: Cape Canaveral, United States ETR / launch complex 12
NASA Center: Jet Propulsion Laboratory
Spacecraft Mass: 202.8 kg
Spacecraft Instruments: 1) microwave radiometer 2) infrared radiometer 3) fluxgate magnetometer 4) cosmic dust detector 5) solar plasma spectrometer and 6) energetic particle detectors
Spacecraft Dimensions: 202.8 kg
Total Cost: Total research, development, launch, and support costs for the Mariner series of spacecraft (Mariners 1 through 10) was approximately $554 million.
Deep Space Chronicle: A Chronology of Deep Space and Planetary Probes 1958-2000, Monographs in Aerospace History No. 24, by Asif A. Siddiqi
National Space Science Data Center, http://nssdc.gsfc.nasa.gov/
After approval by NASA Headquarters in September 1961, JPL prepared three spacecraft based on the design of the Ranger Block I series (therefore named Mariner R) to fly by Venus in late 1962.
Each spacecraft carried a modest suite (9 kilograms) of scientific instrumentation but had no imaging capability. The spacecraft included 54,000 components and was designed to maintain contact with Earth for 2,500 hours -- an ambitious goal given that the (still unsuccessful) Ranger was designed for only 65 hours of contact.
Mariner 1 would have flown by Venus at a range of 29,000 kilometers on 8 December 1962, but due to an incorrect trajectory during launch, range safety had to destroy the booster and its payload at T+290 seconds.