Mars atmospheric entry

Mars atmospheric entry is the entry into the atmosphere of Mars . High velocity entry into Martian air creates a CO 2 -N 2 plasma, as opposed to O 2 -N 2 for Earth air. [1] Mars entry is affected by the radiative effects of hot CO 2 gas and Martian dust suspended in the air. [2] Flight regimes for entry, descent, and landing systems include aerocapture, hypersonic, supersonic, and subsonic. [3]

Page Revisions

Year Metadata Sections Top Words First Paragraph
2018

51955 characters

10 sections

12 paragraphs

11 images

49 internal links

19 external links

1. Overview

2. List of spacecraft

3. Technologies

4. Examples

5. Landing site identification

6. See also

7. References

8. Further reading

entry 0.442

isotensoid 0.248

retropropulsion 0.248

descent 0.183

cone 0.173

landing 0.160

tension 0.153

retropropulsive 0.140

velocity 0.139

supersonic 0.133

spacex 0.133

fence 0.128

aerocapture 0.128

torus 0.112

stacked 0.105

Mars atmospheric entry is the entry into the atmosphere of Mars . High velocity entry into Martian air creates a CO 2 -N 2 plasma, as opposed to O 2 -N 2 for Earth air. [1] Mars entry is affected by the radiative effects of hot CO 2 gas and Martian dust suspended in the air. [2] Flight regimes for entry, descent, and landing systems include aerocapture, hypersonic, supersonic, and subsonic. [3]

2017

37197 characters

9 sections

10 paragraphs

8 images

42 internal links

13 external links

1. Overview

2. List of spacecraft

3. Technologies

4. Examples

5. See also

6. References

7. Further reading

entry 0.465

isotensoid 0.260

retropropulsion 0.260

descent 0.192

cone 0.182

tension 0.161

supersonic 0.139

fence 0.134

aerocapture 0.134

landing 0.131

torus 0.117

velocity 0.117

stacked 0.111

parachute 0.109

n2 0.107

Mars atmospheric entry is the entry into the atmosphere of Mars . High velocity entry into Martian air creates a CO 2 -N 2 plasma, as opposed to O 2 -N 2 for Earth air. [1] Mars entry is affected by the radiative effects of hot CO 2 gas and Martian dust suspended in the air. [2] Flight regimes for entry, descent, and landing systems include aerocapture, hypersonic, supersonic, and subsonic. [3]

2016

36340 characters

7 sections

10 paragraphs

8 images

42 internal links

13 external links

1. Examples

2. Technologies

3. Example (Mars Science Laboratory)

4. Mars Pathfinder EDL

5. See also

6. References

7. Further reading

entry 0.465

isotensoid 0.260

retropropulsion 0.260

descent 0.192

cone 0.182

tension 0.161

supersonic 0.139

fence 0.134

aerocapture 0.134

landing 0.131

torus 0.117

velocity 0.117

stacked 0.111

parachute 0.109

n2 0.107

Mars atmospheric entry is the entry into the atmosphere of Mars . High velocity entry into Martian air creates a CO 2 -N 2 plasma, as opposed to O 2 -N 2 for Earth air. [1] Mars entry is affected by the radiative effects of hot CO 2 gas and Martian dust suspended in the air. [2] Flight regimes for entry, descent, and landing systems include aerocapture, hypersonic, supersonic, and subsonic. [3]

2015

34376 characters

6 sections

9 paragraphs

6 images

39 internal links

12 external links

1. Examples

2. Technologies

3. Example

4. See also

5. References

6. Further reading

entry 0.464

isotensoid 0.260

retropropulsion 0.260

descent 0.192

cone 0.182

tension 0.161

supersonic 0.139

fence 0.134

aerocapture 0.134

landing 0.131

torus 0.117

velocity 0.117

stacked 0.111

parachute 0.109

n2 0.107

Mars atmospheric entry is the entry into the atmosphere of Mars . High velocity entry into Martian air creates a CO 2 -N 2 plasma, as opposed to O 2 -N 2 for Earth air. [1] Mars entry is effected by the radiative effects of hot CO 2 gas and Martian dust suspended in the air. [2] Flight regimes for entry, descent, and landing systems include aerocapture, hypersonic, supersonic, and subsonic. [3]

2014

34268 characters

6 sections

9 paragraphs

6 images

38 internal links

12 external links

1. Examples

2. Technologies

3. Example

4. See also

5. References

6. Further reading

entry 0.464

isotensoid 0.260

retropropulsion 0.260

descent 0.192

cone 0.182

tension 0.161

supersonic 0.139

fence 0.134

aerocapture 0.134

landing 0.131

torus 0.117

velocity 0.117

stacked 0.111

parachute 0.109

n2 0.107

Mars atmospheric entry is the entry into the atmosphere of Mars . High velocity entry into Martian air creates a CO 2 -N 2 plasma, as opposed to O 2 -N 2 for Earth air. [1] Mars entry is effected by the radiative effects of hot CO 2 gas and Martian dust suspended in the air. [2] Flight regimes for entry, descent, and landing systems include aerocapture, hypersonic, supersonic, and subsonic. [3]

2013

20181 characters

6 sections

7 paragraphs

6 images

27 internal links

11 external links

1. Examples

2. Technologies

3. Example

4. See also

5. References

6. Further reading

entry 0.427

isotensoid 0.326

cone 0.229

tension 0.202

fence 0.168

aerocapture 0.168

torus 0.147

stacked 0.139

parachute 0.137

n2 0.134

inflatable 0.133

timeline 0.124

descent 0.120

air 0.120

supersonic 0.116

Mars atmospheric entry is the entry into the atmosphere of Mars . High velocity entry into Martian air creates a CO 2 -N 2 plasma, as opposed to O 2 -N 2 for Earth air. [1] Mars entry is effected by the radiative effects of hot CO 2 gas and Martian dust suspended in the air. [2] Flight regimes for entry, descent, and landing systems include aerocapture, hypersonic, supersonic, and subsonic. [3]

2012

18338 characters

6 sections

7 paragraphs

5 images

24 internal links

10 external links

1. Examples

2. Technologies

3. Example

4. References

5. Further reading

6. See also

entry 0.427

isotensoid 0.326

cone 0.229

tension 0.202

fence 0.168

aerocapture 0.168

torus 0.147

stacked 0.139

parachute 0.137

n2 0.134

inflatable 0.133

timeline 0.124

descent 0.120

air 0.120

supersonic 0.116

Mars atmospheric entry is the entry into the atmosphere of Mars . High velocity entry into Martian air creates a CO 2 -N 2 plasma, as opposed to O 2 -N 2 for Earth air. [1] Mars entry is effected by the radiative effects of hot CO 2 gas and Martian dust suspended in the air. [2] Flight regimes for entry, descent, and landing systems include aerocapture, hypersonic, supersonic, and subsonic. [3]