This presentation deals with current space congestion scenario and the available measures that could be taken to cope with the continually emerging problem.
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Space Debris Removal System
1. Department of Electronics and
Communication Engineering (ECE)
SPACE DEBRIS REMOVAL
SYSTEM
Krishna Institute of Engineering
and Technology
Mohammad Shadab
University Roll No 1302931086
Presented By:- Presented To:
Shipra &Saumya MAM
2. Introduction
Types of orbits
Sources of debris
Tracking and Measurement
of Space Debris
Mitigation of Space Debris
Conclusion
Points of Discussion
4. INTRODUCTION
Space Debris , also known as orbital debris , space junk and
space waste , is the collection of defunct objects in orbit around
Earth.
They can include anything from entire used rocket stages and out
of order satellites to explosion fragments, paint flakes, dust, slag
from solid rocket motors, coolant released by Upravlyaemy
Sputnik Aktivnyj (Russian: Управляемый Спутник
Активный),also known in the west as Radar Ocean
Reconnaissance Satellite or RORSAT other small particles from
equipments.
Debris poses a growing threat to satellites and could prevent the
use of valuable orbits in the future.
5. SPACE SURVEILLANCE NETWORK (SSN)
Debris Size 0.1-1cm 1-10cm >10cm
Total Number at all altitudes 150 million 780,000 23,000
Debris in Low-Earth Orbit 20 million 400,000 15,000
Estimated amount of Space Debris:
Currently more than 15,000 objects are tracked and kept in catalogue by SSN
Space debris number is much more than catalogued
6. Threat of this size?
• Category I (<1cm) - They can make significant
damage to vulnerable parts of a satellite.
• Category II (1-10cm) - They tend to seriously
damage or destroy a satellite in a collision.
• Category III (>10cm) – They may completely
destroy a satellite in a collision and can be
tracked easily.
Categorization:
10. The International Space Station is in an LEO that
varies between 320 km (199 miles) and 400 km
(249 miles) above the Earth's surface.
Hubble Space Telescope
Earth's plates, remote sensing, spatial
investigation, meteorology.
Phone Satellites
Experiments and Installation
Features of LEO:
12. GRAPHIC EVOLUTION OF TRACKABLE LEO
ORBIT OBJECT:
Graphic evolution of total trackable Low-Earth Obit (LEO) object population since 1994
Source: Marshall H. Kaplan, Survey of Space Debris Reduction Methods, AIAA SPACE 2009 Conference & Exposition 14 - 17 September 2009, Pasadena,
California,AIAA 2009-6619
The number of space debris increases very quickly:
16. Altitude -2000 km to 36,000 km
approx.
Common Use :Navigation , GPS
Communication ,MAPS and Space
and Environment science.
Orbital Period –Apogee ,Perigee
Medium Earth Orbit
17. Geostationary Earth Orbit
Altitude - 35786 Km ,Precise and
Calculative.
Television Broadcasting
Weather Forecast-Storm
movements and developments.
NATIONAL SECURITY
18. Highly Elliptical Orbit
These satellites do not follow a circular orbit, but its orbit is elliptical.
Its orbital period is of 8 to 24 hours.
The perigee about 500 km and apogee of 50000 km.
Fig. HEO
24. Laser brooms
Fast
Direct Impact
Drag by photon force
Technology is mature
• Could not be move freely in a huge range
• Threat- Space based weapon system
26. Solar sails
Principle
Outer Orbit Reach
No propellant or engines
Less maintenance
• Difficult to control
• Deployment
• Crashes
27. Space Nets and
Collector satellites
Space nets or umbrellas are
satellites which eject a huge net
that ‘fishes’ or collects the debris
and is later disposed off into a
graveyard orbit .
Uses momentum generated through
throwing for movement