Mars 2MV-3 No.1

Mars 2MV-3 No.1 [1] [2] also known as Sputnik 24 in the West, was a Soviet spacecraft, which was launched in 1962 as part of the Mars program , and was intended to land on the surface of Mars . [3] [4] Due to a problem with the rocket which launched it, it did not depart low Earth orbit , [5] and it decayed several days later. It was the only Mars 2MV-3 spacecraft to be launched. [2]

Page Revisions

Year Metadata Sections Top Words First Paragraph
2018

61409 characters

4 sections

3 paragraphs

6 images

250 internal links

15 external links

1. Launch

2. Designation

3. See also

4. References

sputnik 0.260

cavitation 0.242

stage 0.239

2mv 0.225

problem 0.217

decayed 0.203

feed 0.188

designations 0.178

depart 0.173

orbit 0.169

upper 0.155

1962 0.149

spacecraft 0.148

launched 0.146

rocket 0.135

Mars 2MV-3 No.1 [1] [2] also known as Sputnik 24 in the West, was a Soviet spacecraft, which was launched in 1962 as part of the Mars program , and was intended to land on the surface of Mars . [3] [4] Due to a problem with the rocket which launched it, it did not depart low Earth orbit , [5] and it decayed several days later. It was the only Mars 2MV-3 spacecraft to be launched. [2]

2017

61009 characters

4 sections

3 paragraphs

6 images

250 internal links

13 external links

1. Launch

2. Designation

3. See also

4. References

sputnik 0.260

cavitation 0.242

stage 0.239

2mv 0.225

problem 0.217

decayed 0.203

feed 0.188

designations 0.178

depart 0.173

orbit 0.169

upper 0.155

1962 0.149

spacecraft 0.148

launched 0.146

rocket 0.135

Mars 2MV-3 No.1 [1] [2] also known as Sputnik 24 in the West, was a Soviet spacecraft, which was launched in 1962 as part of the Mars program , and was intended to land on the surface of Mars . [3] [4] Due to a problem with the rocket which launched it, it did not depart low Earth orbit , [5] and it decayed several days later. It was the only Mars 2MV-3 spacecraft to be launched. [2]

2016

60434 characters

4 sections

3 paragraphs

6 images

250 internal links

10 external links

1. Launch

2. Designation

3. See also

4. References

sputnik 0.260

cavitation 0.242

stage 0.239

2mv 0.225

problem 0.217

decayed 0.203

feed 0.188

designations 0.178

depart 0.173

orbit 0.169

upper 0.155

1962 0.149

spacecraft 0.148

launched 0.146

rocket 0.135

Mars 2MV-3 No.1 [1] [2] also known as Sputnik 24 in the West, was a Soviet spacecraft, which was launched in 1962 as part of the Mars program , and was intended to land on the surface of Mars . [3] [4] Due to a problem with the rocket which launched it, it did not depart low Earth orbit , [5] and it decayed several days later. It was the only Mars 2MV-3 spacecraft to be launched. [2]

2014

59132 characters

3 sections

3 paragraphs

6 images

250 internal links

10 external links

1. Launch

2. Designation

3. References

sputnik 0.260

cavitation 0.242

stage 0.239

2mv 0.225

problem 0.217

decayed 0.203

feed 0.188

designations 0.178

depart 0.173

orbit 0.169

upper 0.155

1962 0.149

spacecraft 0.148

launched 0.146

rocket 0.135

Mars 2MV-3 No.1 [1] [2] also known as Sputnik 24 in the West, was a Soviet spacecraft, which was launched in 1962 as part of the Mars program , and was intended to land on the surface of Mars . [3] [4] Due to a problem with the rocket which launched it, it did not depart low Earth orbit , [5] and it decayed several days later. It was the only Mars 2MV-3 spacecraft to be launched. [2]

2013

77331 characters

1 sections

3 paragraphs

7 images

374 internal links

10 external links

1. References

2mv 0.320

sputnik 0.247

cavitation 0.229

stage 0.226

problem 0.206

decayed 0.193

feed 0.178

designations 0.169

depart 0.165

orbit 0.161

upper 0.147

1962 0.141

spacecraft 0.141

launched 0.138

890 0.134

Mars 2MV-3 No.1 [1] [2] also known as Sputnik 24 in the West, was a Soviet spacecraft, which was launched in 1962 as part of the Mars program , and was intended to land on the surface of Mars . [3] [4] Due to a problem with the rocket which launched it, it did not depart low Earth orbit , [5] and it decayed several days later. It was the only Mars 2MV-3 spacecraft to be launched. [2]

2012

53573 characters

1 sections

4 paragraphs

4 images

250 internal links

8 external links

1. References

2mv 0.320

sputnik 0.246

cavitation 0.229

stage 0.226

problem 0.205

decayed 0.192

feed 0.178

designations 0.169

depart 0.164

orbit 0.160

upper 0.147

1962 0.141

spacecraft 0.140

launched 0.138

890 0.133

Mars 2MV-3 No.1 [1] [2] also known as Sputnik 24 in the West, was a Soviet spacecraft, which was launched in 1962 as part of the Mars programme , and was intended to land on the surface of Mars . [3] [4] Due to a problem with the rocket which launched it, it did not depart low Earth orbit , [5] and it decayed several days later. It was the only Mars 2MV-3 spacecraft to be launched. [2]

2011

53563 characters

1 sections

3 paragraphs

4 images

250 internal links

8 external links

1. References

2mv 0.320

sputnik 0.246

cavitation 0.229

stage 0.226

problem 0.205

decayed 0.192

feed 0.178

designations 0.169

depart 0.164

orbit 0.160

upper 0.147

1962 0.141

spacecraft 0.140

launched 0.138

890 0.133

Mars 2MV-3 No.1 [1] [2] also known as Sputnik 24 in the West, was a Soviet spacecraft, which was launched in 1962 as part of the Mars programme , and was intended to land on the surface of Mars . [3] [4] Due to a problem with the rocket which launched it, it did not depart low Earth orbit , [5] and it decayed several days later. It was the only Mars 2MV-3 spacecraft to be launched. [2]

2010

53557 characters

1 sections

3 paragraphs

4 images

250 internal links

8 external links

1. References

2mv 0.320

sputnik 0.246

cavitation 0.229

stage 0.226

problem 0.205

decayed 0.192

feed 0.178

designations 0.169

depart 0.164

orbit 0.160

upper 0.147

1962 0.141

spacecraft 0.140

launched 0.138

890 0.133

Mars 2MV-3 No.1 [1] [2] also known as Sputnik 24 in the West, was a Soviet spacecraft, which was launched in 1962 as part of the Mars programme , and was intended to land on the surface of Mars . [3] [4] Due to a problem with the rocket which launched it, it did not depart low Earth orbit , [5] and it decayed several days later. It was the only Mars 2MV-3 spacecraft to be launched. [2]

2009

28498 characters

1 sections

3 paragraphs

5 images

139 internal links

0 external links

1. See also

sputnik 0.360

booster 0.304

decayed 0.280

6500 0.230

1962b 0.194

890 0.194

sl 0.185

korabl 0.178

xi 0.172

spacecraft 0.171

590 0.155

warning 0.147

beta 0.142

197 0.136

tracked 0.135

Sputnik 24 (also known as Beta Xi 1 , Korabl 13 , and Mars 1962B ) was an attempted Mars lander mission. The SL-6/A-2-e launcher put the spacecraft and the attached booster upper stage into a 197 × 590 km Earth orbit with an inclination of 64.7 degrees. The total mass of the booster/spacecraft complex (the Tyazheliy Sputnik) was roughly 6500 kg, the Mars spacecraft component comprising about 890 kg of this. The complex broke up during the burn to transfer to Mars trajectory. Five large pieces were tracked by the U.S. Ballistic Missile Early Warning System. The geocentric orbit of the presumed booster decayed on 25 December 1962 and the Mars spacecraft orbit decayed and it re-entered Earth's atmosphere on January 19, 1963.

2008

27015 characters

1 sections

2 paragraphs

4 images

138 internal links

0 external links

1. See also

sputnik 0.360

booster 0.304

decayed 0.280

6500 0.230

1962b 0.194

890 0.194

sl 0.185

korabl 0.178

xi 0.172

spacecraft 0.171

590 0.155

warning 0.147

beta 0.142

197 0.136

tracked 0.135

Sputnik 24 (also known as Beta Xi 1 , Korabl 13 , and Mars 1962B ) was an attempted Mars lander mission. The SL-6/A-2-e launcher put the spacecraft and the attached booster upper stage into a 197 × 590 km Earth orbit with an inclination of 64.7 degrees. The total mass of the booster/spacecraft complex (the Tyazheliy Sputnik) was roughly 6500 kg, the Mars spacecraft component comprising about 890 kg of this. The complex broke up during the burn to transfer to Mars trajectory. Five large pieces were tracked by the U.S. Ballistic Missile Early Warning System. The geocentric orbit of the presumed booster decayed on 25 December 1962 and the Mars spacecraft orbit decayed and it re-entered Earth's atmosphere on January 19 , 1963 .

2007

25289 characters

1 sections

2 paragraphs

3 images

133 internal links

0 external links

1. See also

sputnik 0.360

booster 0.304

decayed 0.280

6500 0.230

1962b 0.194

890 0.194

sl 0.185

korabl 0.178

xi 0.172

spacecraft 0.171

590 0.155

warning 0.147

beta 0.142

197 0.136

tracked 0.135

Sputnik 24 (also known as Beta Xi 1 , Korabl 13 , and Mars 1962B ) was an attempted Mars lander mission. The SL-6/A-2-e launcher put the spacecraft and the attached booster upper stage into a 197 × 590 km Earth orbit with an inclination of 64.7 degrees. The total mass of the booster/spacecraft complex (the Tyazheliy Sputnik) was roughly 6500 kg, the Mars spacecraft component comprising about 890 kg of this. The complex broke up during the burn to transfer to Mars trajectory. Five large pieces were tracked by the U.S. Ballistic Missile Early Warning System. The geocentric orbit of the presumed booster decayed on 25 December 1962 and the Mars spacecraft orbit decayed and it re-entered Earth's atmosphere on January 19 , 1963 .

2006

25289 characters

1 sections

2 paragraphs

3 images

133 internal links

0 external links

1. See also

sputnik 0.360

booster 0.304

decayed 0.280

6500 0.230

1962b 0.194

890 0.194

sl 0.185

korabl 0.178

xi 0.172

spacecraft 0.171

590 0.155

warning 0.147

beta 0.142

197 0.136

tracked 0.135

Sputnik 24 (also known as Beta Xi 1 , Korabl 13 , and Mars 1962B ) was an attempted Mars lander mission. The SL-6/A-2-e launcher put the spacecraft and the attached booster upper stage into a 197 × 590 km Earth orbit with an inclination of 64.7 degrees. The total mass of the booster/spacecraft complex (the Tyazheliy Sputnik) was roughly 6500 kg, the Mars spacecraft component comprising about 890 kg of this. The complex broke up during the burn to transfer to Mars trajectory. Five large pieces were tracked by the U.S. Ballistic Missile Early Warning System. The geocentric orbit of the presumed booster decayed on 25 December 1962 and the Mars spacecraft orbit decayed and it re-entered Earth's atmosphere on January 19 , 1963 .

2005

2600 characters

1 sections

2 paragraphs

0 images

10 internal links

0 external links

1. Related articles

sputnik 0.360

booster 0.304

decayed 0.280

6500 0.230

1962b 0.194

890 0.194

sl 0.185

korabl 0.178

xi 0.172

spacecraft 0.171

590 0.155

warning 0.147

beta 0.142

197 0.136

tracked 0.135

Sputnik 24 (also known as Beta Xi 1 , Korabl 13 , and Mars 1962B ) was an attempted Mars lander mission. The SL-6/A-2-e launcher put the spacecraft and the attached booster upper stage into a 197 × 590 km Earth orbit with an inclination of 64.7 degrees. The total mass of the booster/spacecraft complex (the Tyazheliy Sputnik) was roughly 6500 kg, the Mars spacecraft component comprising about 890 kg of this. The complex broke up during the burn to transfer to Mars trajectory. Five large pieces were tracked by the U.S. Ballistic Missile Early Warning System. The geocentric orbit of the presumed booster decayed on 25 December 1962 and the Mars spacecraft orbit decayed and it re-entered Earth's atmosphere on January 19 , 1963 .

2004

2494 characters

1 sections

2 paragraphs

0 images

8 internal links

0 external links

1. Related articles

sputnik 0.360

booster 0.304

decayed 0.280

6500 0.230

1962b 0.194

890 0.194

sl 0.185

korabl 0.178

xi 0.172

spacecraft 0.171

590 0.155

warning 0.147

beta 0.142

197 0.136

tracked 0.135

Sputnik 24 (also known as Beta Xi 1 , Korabl 13 , and Mars 1962B ) was an attempted Mars lander mission. The SL-6/A-2-e launcher put the spacecraft and the attached booster upper stage into a 197 × 590 km Earth orbit with an inclination of 64.7 degrees. The total mass of the booster/spacecraft complex (the Tyazheliy Sputnik) was roughly 6500 kg, the Mars spacecraft component comprising about 890 kg of this. The complex broke up during the burn to transfer to Mars trajectory. Five large pieces were tracked by the U.S. Ballistic Missile Early Warning System. The geocentric orbit of the presumed booster decayed on 25 December 1962 and the Mars spacecraft orbit decayed and it re-entered Earth's atmosphere on January 19 , 1963 .

2002

1777 characters

0 sections

2 paragraphs

0 images

5 internal links

0 external links

sputnik 0.384

booster 0.325

decayed 0.299

6500 0.246

890 0.208

sl 0.198

spacecraft 0.182

590 0.166

warning 0.157

197 0.146

tracked 0.144

geocentric 0.136

missile 0.136

naval 0.133

summary 0.129

Sputnik 24 was an attempted Mars lander mission. The SL-6/A-2-e launcher put the spacecraft and the attached booster upper stage into a 197 x 590 km Earth orbit with an inclination of 64.7 degrees. The total mass of the booster/spacecraft complex (the Tyazheliy Sputnik) was roughly 6500 kg, the Mars spacecraft component comprising about 890 kg of this. The complex broke up during the burn to transfer to Mars trajectory. Five large pieces were tracked by the U.S. Ballistic Missile Early Warning System. The geocentric orbit of the presumed booster decayed on 25 December 1962 and the Mars spacecraft orbit decayed and it re-entered Earth's atmosphere on January 19 , 1963 .