Mars 1
Mars 1 , also known as 1962 Beta Nu 1 , Mars 2MV-4 and Sputnik 23 , was an automatic interplanetary station launched in the direction of Mars on November 1, 1962, [1] [2] the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km (6,800 mi). It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field, radiation environment, atmospheric structure, and possible organic compounds. [1] [2]
Page Revisions
| Year | Metadata | Sections | Top Words | First Paragraph |
| 2018 |
66437 characters 6 sections 7 paragraphs 9 images 255 internal links 7 external links |
antenna 0.273 transmitter 0.229 ft 0.220 2mv 0.217 cylinder 0.209 module 0.206 mounted 0.185 sputnik 0.167 radiators 0.160 wavelength 0.154 spacecraft 0.143 1m 0.137 micrometeoroid 0.132 omnidirectional 0.125 panels 0.116 |
Mars 1 , also known as 1962 Beta Nu 1 , Mars 2MV-4 and Sputnik 23 , was an automatic interplanetary station launched in the direction of Mars on November 1, 1962, [1] [2] the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km (6,800 mi). It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field, radiation environment, atmospheric structure, and possible organic compounds. [1] [2] |
|
| 2017 |
66233 characters 6 sections 7 paragraphs 9 images 254 internal links 7 external links |
antenna 0.273 transmitter 0.229 ft 0.220 2mv 0.217 cylinder 0.209 module 0.206 mounted 0.185 sputnik 0.167 radiators 0.160 wavelength 0.154 spacecraft 0.143 1m 0.137 micrometeoroid 0.132 omnidirectional 0.125 panels 0.116 |
Mars 1 , also known as 1962 Beta Nu 1 , Mars 2MV-4 and Sputnik 23 , was an automatic interplanetary station launched in the direction of Mars on November 1, 1962, [1] [2] the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km (6,800 mi). It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field, radiation environment, atmospheric structure, and possible organic compounds. [1] [2] |
|
| 2016 |
65987 characters 6 sections 7 paragraphs 9 images 254 internal links 6 external links |
antenna 0.273 transmitter 0.229 ft 0.220 2mv 0.217 cylinder 0.209 module 0.206 mounted 0.185 sputnik 0.167 radiators 0.160 wavelength 0.154 spacecraft 0.143 1m 0.137 micrometeoroid 0.132 omnidirectional 0.125 panels 0.116 |
Mars 1 , also known as 1962 Beta Nu 1 , Mars 2MV-4 and Sputnik 23 , was an automatic interplanetary station launched in the direction of Mars on November 1, 1962, [1] [2] the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km (6,800 mi). It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field, radiation environment, atmospheric structure, and possible organic compounds. [1] [2] |
|
| 2015 |
65481 characters 6 sections 6 paragraphs 9 images 253 internal links 6 external links |
antenna 0.282 transmitter 0.236 ft 0.227 cylinder 0.215 module 0.212 mounted 0.191 sputnik 0.172 radiators 0.165 wavelength 0.159 2mv 0.149 spacecraft 0.147 micrometeoroid 0.136 omnidirectional 0.129 panels 0.120 experiment 0.113 |
Mars 1 , also known as 1962 Beta Nu 1 , Mars 2MV-4 and Sputnik 23 , was an automatic interplanetary station launched in the direction of Mars on November 1, 1962, [1] [2] the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km (6,800 mi). It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field, radiation environment, atmospheric structure, and possible organic compounds. [1] [2] |
|
| 2014 |
60772 characters 6 sections 5 paragraphs 7 images 255 internal links 2 external links |
antenna 0.258 transmitter 0.217 ft 0.208 cylinder 0.197 000 0.195 module 0.194 mounted 0.175 sputnik 0.158 radiators 0.151 wavelength 0.146 nt 0.143 2mv 0.137 spacecraft 0.135 micrometeoroid 0.125 omnidirectional 0.118 |
Mars 1 , also known as 1962 Beta Nu 1 , Mars 2MV-4 and Sputnik 23 , was an automatic interplanetary station launched in the direction of Mars on November 1, 1962, [1] [2] the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km (6,800 mi). It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field, radiation environment, atmospheric structure, and possible organic compounds. [1] [2] After leaving Earth orbit , the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at five days in which a large amount of interplanetary data were collected. [1] On 21 March 1963, when the spacecraft was at a distance of 106,760,000 km (66,340,000 mi) from Earth on its way to Mars, communications ceased, probably due to failure of the spacecraft's antenna orientation system. [1] [2] Mars 1 closest approach to Mars occurred on June 19, 1963 at a distance of approximately 193,000 km (120,000 mi), after which the spacecraft entered an orbit around the Sun . [2] |
|
| 2013 |
54893 characters 5 sections 5 paragraphs 4 images 258 internal links 1 external links |
citation 0.271 antenna 0.252 needed 0.236 transmitter 0.212 cylinder 0.193 module 0.190 mounted 0.171 sputnik 0.154 radiators 0.148 wavelength 0.142 nt 0.140 radiation 0.135 2mv 0.133 spacecraft 0.132 micrometeoroid 0.122 |
Mars 1 , also known as 1962 Beta Nu 1 , Mars 2MV-4 and Sputnik 23 , was an automatic interplanetary station launched in the direction of Mars on November 1, 1962, [ citation needed ] the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km . It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field , radiation environment, atmospheric structure, and possible organic compounds. [ citation needed ] After leaving Earth orbit , the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at five days in which a large amount of interplanetary data were collected. [ citation needed ] On 21 March 1963, when the spacecraft was at a distance of 106,760,000 km from Earth on its way to Mars, communications ceased, [ citation needed ] probably due to failure of the spacecraft's antenna orientation system. [ citation needed ] Mars 1 closest approach to Mars occurred on June 19, 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit . |
|
| 2012 |
51643 characters 5 sections 5 paragraphs 4 images 253 internal links 1 external links |
citation 0.270 antenna 0.252 needed 0.235 transmitter 0.211 cylinder 0.192 module 0.190 mounted 0.171 sputnik 0.154 radiators 0.148 wavelength 0.142 nt 0.140 radiation 0.135 2mv 0.133 spacecraft 0.132 micrometeoroid 0.122 |
Mars 1 , also known as 1962 Beta Nu 1 , Mars 2MV-4 and Sputnik 23 , was an automatic interplanetary station launched in the direction of Mars on November 1, 1962, [ citation needed ] the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km . It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field , radiation environment, atmospheric structure, and possible organic compounds. [ citation needed ] After leaving Earth orbit , the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at five days in which a large amount of interplanetary data were collected. [ citation needed ] On 21 March 1963, when the spacecraft was at a distance of 106,760,000 km from Earth on its way to Mars, communications ceased, [ citation needed ] probably due to failure of the spacecraft's antenna orientation system. [ citation needed ] Mars 1 closest approach to Mars occurred on June 19, 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit . |
|
| 2011 |
46538 characters 5 sections 5 paragraphs 4 images 246 internal links 1 external links |
antenna 0.272 transmitter 0.228 cylinder 0.208 module 0.205 mounted 0.184 sputnik 0.166 radiators 0.159 wavelength 0.154 nt 0.151 2mv 0.144 spacecraft 0.142 micrometeoroid 0.132 omnidirectional 0.125 radiation 0.116 panels 0.116 |
Mars 1 , also known as 1962 Beta Nu 1 , Mars 2MV-4 and Sputnik 23 , was an automatic interplanetary station launched in the direction of Mars on November 1, 1962, the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km . It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field , radiation environment, atmospheric structure, and possible organic compounds. After leaving Earth orbit , the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at five days in which a large amount of interplanetary data were collected. On 21 March 1963, when the spacecraft was at a distance of 106,760,000 km from Earth on its way to Mars, communications ceased, probably due to failure of the spacecraft's antenna orientation system. Mars 1 closest approach to Mars occurred on June 19, 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit . |
|
| 2010 |
46309 characters 5 sections 5 paragraphs 4 images 246 internal links 1 external links |
antenna 0.271 transmitter 0.228 cylinder 0.207 module 0.204 mounted 0.184 sputnik 0.166 radiators 0.159 wavelength 0.153 nt 0.150 2mv 0.144 spacecraft 0.142 micrometeoroid 0.131 omnidirectional 0.124 centimeter 0.121 radiation 0.116 |
Mars 1 , also known as 1962 Beta Nu 1 , Mars 2MV-4 and Sputnik 23 , was an automatic interplanetary station launched in the direction of Mars on November 1, 1962, the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km . It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field , radiation environment, atmospheric structure, and possible organic compounds. After leaving Earth orbit , the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at five days in which a large amount of interplanetary data were collected. On 21 March 1963, when the spacecraft was at a distance of 106,760,000 km from Earth on its way to Mars, communications ceased, probably due to failure of the spacecraft's antenna orientation system. Mars 1 closest approach to Mars occurred on June 19, 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit . |
|
| 2009 |
33296 characters 5 sections 5 paragraphs 4 images 148 internal links 1 external links |
antenna 0.271 transmitter 0.228 cylinder 0.207 module 0.204 mounted 0.184 sputnik 0.166 radiators 0.159 wavelength 0.153 nt 0.150 2mv 0.144 spacecraft 0.142 micrometeoroid 0.131 omnidirectional 0.124 centimeter 0.121 radiation 0.116 |
Mars 1 , also known as 1962 Beta Nu 1 , Mars 2MV-4 and Sputnik 23 , was an automatic interplanetary station launched in the direction of Mars on November 1, 1962, the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km . It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field , radiation environment, atmospheric structure, and possible organic compounds. After leaving Earth orbit , the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at five days in which a large amount of interplanetary data were collected. On 21 March 1963, when the spacecraft was at a distance of 106,760,000 km from Earth on its way to Mars, communications ceased, probably due to failure of the spacecraft's antenna orientation system. Mars 1 closest approach to Mars occurred on June 19, 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit . |
|
| 2008 |
33869 characters 5 sections 6 paragraphs 5 images 153 internal links 1 external links |
antenna 0.271 transmitter 0.228 cylinder 0.207 module 0.204 mounted 0.184 sputnik 0.166 radiators 0.159 wavelength 0.153 nt 0.150 2mv 0.144 spacecraft 0.142 micrometeoroid 0.131 omnidirectional 0.124 centimeter 0.121 radiation 0.116 |
Mars 1 , also known as 1962 Beta Nu 1 , Mars 2MV-4 and Sputnik 23 , was an automatic interplanetary station launched in the direction of Mars on November 1 , 1962 , the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km . It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field , radiation environment, atmospheric structure, and possible organic compounds. After leaving Earth orbit , the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at five days in which a large amount of interplanetary data were collected. On 21 March 1963 , when the spacecraft was at a distance of 106,760,000 km from Earth on its way to Mars, communications ceased, probably due to failure of the spacecraft's antenna orientation system. Mars 1 closest approach to Mars occurred on June 19 , 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit . |
|
| 2007 |
30301 characters 3 sections 5 paragraphs 4 images 148 internal links 0 external links |
antenna 0.276 transmitter 0.232 cylinder 0.211 module 0.208 mounted 0.187 radiators 0.162 wavelength 0.156 nt 0.153 spacecraft 0.144 micrometeoroid 0.134 omnidirectional 0.127 centimeter 0.124 radiation 0.118 panels 0.118 sputnik 0.113 |
Mars 1 (1962 Beta Nu 1) was an automatic interplanetary station launched in the direction of Mars on November 1 , 1962 , the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km . It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field , radiation environment, atmospheric structure, and possible organic compounds. After leaving Earth orbit , the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at five days in which a large amount of interplanetary data were collected. On 21 March 1963 , when the spacecraft was at a distance of 106,760,000 km from Earth on its way to Mars, communications ceased, probably due to failure of the spacecraft's antenna orientation system. Mars 1 closest approach to Mars occurred on June 19 , 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit . |
|
| 2006 |
30262 characters 3 sections 5 paragraphs 4 images 148 internal links 0 external links |
antenna 0.276 transmitter 0.232 cylinder 0.211 module 0.208 mounted 0.187 radiators 0.162 wavelength 0.156 nt 0.153 spacecraft 0.144 micrometeoroid 0.134 omnidirectional 0.127 centimeter 0.123 radiation 0.118 panels 0.118 sputnik 0.113 |
Mars 1 (1962 Beta Nu 1) was an automatic interplanetary station launched in the direction of Mars on November 1 , 1962 , the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km . It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field , radiation environment, atmospheric structure, and possible organic compounds. After leaving Earth orbit , the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at 5 days in which a large amount of interplanetary data were collected. On 21 March 1963 , when the spacecraft was at a distance of 106,760,000 km from Earth on its way to Mars, communications ceased, probably due to failure of the spacecraft's antenna orientation system. Mars 1 closest approach to Mars occurred on June 19 , 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit . |
|
| 2005 |
7031 characters 3 sections 5 paragraphs 0 images 24 internal links 0 external links |
antenna 0.276 transmitter 0.232 cylinder 0.211 module 0.208 mounted 0.187 radiators 0.162 wavelength 0.156 nt 0.153 spacecraft 0.144 micrometeoroid 0.134 omnidirectional 0.127 centimeter 0.123 radiation 0.118 panels 0.118 sputnik 0.113 |
Mars 1 (1962 Beta Nu 1) was an automatic interplanetary station launched in the direction of Mars on November 1 , 1962 , the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km . It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field , radiation environment, atmospheric structure, and possible organic compounds. After leaving Earth orbit , the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at 5 days in which a large amount of interplanetary data were collected. On 21 March 1963 , when the spacecraft was at a distance of 106,760,000 km from Earth on its way to Mars, communications ceased, probably due to failure of the spacecraft's antenna orientation system. Mars 1 closest approach to Mars occurred on June 19 , 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit . |
|
| 2004 |
6653 characters 3 sections 5 paragraphs 0 images 19 internal links 0 external links |
transmitter 0.240 antenna 0.238 cylinder 0.218 module 0.215 mounted 0.194 radiators 0.167 wavelength 0.161 spacecraft 0.149 micrometeoroid 0.138 omnidirectional 0.131 centimeter 0.128 radiation 0.122 panels 0.122 sputnik 0.117 experiment 0.115 |
Mars 1 (1962 Beta Nu 1) was an automatic interplanetary station launched in the direction of Mars , the first of the Soviet Mars probe program , with the intent of flying by the planet at a distance of about 11,000 km. It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field , radiation environment, atmospheric structure, and possible organic compounds. After leaving Earth orbit , the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at 5 days in which a large amount of interplanetary data were collected. On 21 March 1963, when the spacecraft was at a distance of 106,760,000 km from Earth on its way to Mars communications ceased, probably due to failure of the spacecraft orientation system. Mars 1 closest approach to Mars occurred on June 19 , 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit . |
|
| 2002 |
5241 characters 2 sections 5 paragraphs 0 images 13 internal links 0 external links |
transmitter 0.240 antenna 0.239 cylinder 0.219 module 0.216 mounted 0.194 radiators 0.168 wavelength 0.162 spacecraft 0.150 micrometeoroid 0.139 omnidirectional 0.131 centimeter 0.128 radiation 0.123 panels 0.122 sputnik 0.117 experiment 0.115 |
Mars 1 (1962 Beta Nu 1) was an automatic interplanetary station launched in the direction of Mars , with the intent of flying by the planet at a distance of about 11,000 km. It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field , radiation environment, atmospheric structure, and possible organic compounds. After leaving Earth orbit , the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at 5 days in which a large amount of interplanetary data were collected. On 21 March 1963, when the spacecraft was at a distance of 106,760,000 km from Earth on its way to Mars communications ceased, probably due to failure of the spacecraft orientation system. Mars 1 closest approach to Mars occurred on June 19 , 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit . |