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NPTEL

Space Environment and its Effects on Orbital Spacecrafts

NPTEL via Swayam

Overview

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ABOUT THE COURSE:The hazardous interactions between the space environment and the orbiting spacecraft may lead to the degradation of spacecraft and its subsystem performance and may lead to the loss of the spacecraft itself. This course aims to provide the students with the introduction to the understanding of different aspects of the space environment, including vacuum environment, neutral particulate environment, space debris, plasma and radiation environment and how these impact on spacecraft design, human and robotic spaceflight, terrestrial infrastructure systems and will enable students to explore a particular topic at a deeper level. Emphasis is laid on problem solving techniques and design guidelines that will provide the student with an understanding of how space environment effects may be minimized through proactive spacecraft design.INTENDED AUDIENCE: Postgraduate and PhD studentsPREREQUISITES: Knowledge of the elementary theories related to Physics and Mathematics and ChemistryINDUSTRY SUPPORT: Indian Space Research Organization.Physical Research Laboratory.The space startups like Pixxel, Dhruva Space, Piersight etc

Syllabus

Week 1: Introduction to Space Environment and Spacecraft Interactions

Lecture 1:Space environment, its types and weather definition, anatomy of Sun, Solar activities as space weather driver
Lecture 2:Solar wind, solar flare, coronal mass ejection, solar energetic particles event.
Lecture 3:Co-rotating Interaction regions, interplanetary magnetic field (IMF).
Lecture 4:Coupling of solar wind to earth’s magnetosphere and ionosphere, geomagnetic storm and substorm, geomagnetic indices.
Lecture 5:Earth’s radiation belt, and ring current, south Atlantic anomaly.
Week 2:Satellite system and its orbit:

Lecture 6:Different types of earth’s orbit for useful satellite applications like LEO, MEO and GEO/GSO, HEO, PEO.
Lecture 7:
Space environment at different earth’s orbits and the applications of the artificial satellites at different orbital altitudes.
Lecture 8:
Satellite space segments 1; Mechanical main frames 1; structures, thermal control system.
Lecture 9:Satellite space segments 1; Mechanical main frames 1; structures, thermal control system.
Lecture 10:Electrical main frames 2; Altitude and orbit control system, station keeping, TT and C, payloads
Week 3:Satellite system:

Lecture 11:
Earth segments 1; Receive-Only Home TV Systems, Transmit-Receive Earth Stations.
Lecture 12:
Earth segments 2;Important subsystems of a typical satellite earth station and Important considerations for satellite operations.

The vacuum spacecraft environment:

Lecture 13:
Characteristics of vacuum environment, heat transfer mechanisms in vacuum and its implication of spacecraft thermal design and challenges.
Lecture 14:
UV radiation exposure of satellites and its effects, out-gassing effects of spacecraft materials, definition of TML, CVCM, WVR and its’ significance.
Lecture 15:
Ground Simulation of vacuum environment, thermo-vacuum chamber, thermo-vacuum test philosophy, Characterization of TML, CVCM and WVR.
Week 4:

Lecture 16:
Material selection, design guidelines and mitigation techniques for vacuum environment.

The neutral environment 1

Lecture 17:Neutral gas flow around a spacecraft, earth’s atmosphere, pressure, density and temperature variation with altitude.
Lecture 18:Planetary atmospheres, aerodynamic force; contamination, erosion by atomic oxygen, spacecraft glow.
Lecture 19:
Particle impacts on spacecraft, scattering of EM radiation from particles.
Lecture 20:
The physics of macroscopic particles, cometary, meteoroids, asteroidal meteors.
Week 5:

Lecture 21:
Spacecraft induced neutral Environments,Spacecraft outgassing; chemical thrusters.
Lecture 22:Space debris, its types, space debris management, monitoring, detection and capturing methods.
Lecture 23:
Simulation, modeling and mitigation techniques for effects neutral environment.

Plasma Environment 1:

Lecture 24:
Basic charged Particle Motion in Constant Electric and Magnetic Fields, gyro-radius, cyclotron frequency.
Lecture 25:
ExB drift, Debye shielding, plasma frequency, magnetic mirroring.
Week 6:Plasma Environment 2:

Lecture 26:
Geomagnetic storm/substorm and the external and disturbance fields
Lecture 27:
Plasma environment in low earth orbit and polar orbits and interaction with spacecrafts
Lecture 28:
The geosynchronous orbit plasma environment; spacecraft-plasma interactions.
Lecture 29:
The physics of spacecraft charging, spacecraft potential.
Lecture 30:Spacecraft surface charging, absolute charging, differential charging
Week 7:Plasma Environment 3

Lecture 31:
General probe theory: the thin-sheath limit, the thick-sheath limit, spacecraft potentials, Langmuir probe.
Lecture 32:
Spacecraft as a Langmuir Probe, Current Collection in spherical, cylindrical and plane geometry
Lecture 33:
Energy distribution of plasma species, Single Maxwellian and double Maxwellian distribution, Spacecraft charging in a Maxwellian plasma
Lecture 34:
Current from the ambient plasma, photoelectric currents, backscattered and secondary electrons.
Lecture 35:
Current balance equation, computation of spacecraft built-up potential.
Week 8:Plasma Environment 3

Lecture 36:
Effect of magnetic fields on current collection, artificial current and charge sources.
Lecture 37:Space Tethers, Plasma Contactors, and Sheath Ionization.
Lecture 38:Electrostatic Discharges on Spacecraft: Location of discharges on spacecraft, differential charging, electromagnetic Interference.
Lecture 39:
Bulk or internal spacecraft charging: high-energyelectron and ion fluxes, penetration of high-energy charges into materials, properties of dielectrics, avalanche ionization in a high electric field.
Lecture 40:
Satellite anomalies due to spacecraft charging, modelling, simulation and testing.
Week 9:Plasma Environment 4

Lecture 41:
Design guide lines and mitigation techniques against spacecraft charging

Radiation environment 1

Lecture 42:Electromagnetic radiation, electromagnetic radiation at radio frequencies, visible and infrared, UV, EUV, and X-rays;
Lecture 43:
Energetic particle radiation; trapped radiation, cosmic rays, Solar proton events.
Lecture 44:
Radiation belts, radiation belt electron population, nominal electron belt structure and dynamics, solar wind drivers of radiation belt dynamics
Lecture 45:
Radiation interactions with matter, single-particle interactions, photon interactions, charged-particle interactions, neutron interactions.
Week 10:Radiation environment 2

Lecture 46:
Space radiation risks to astronauts, case studies of ISS
Lecture 47:Effects on spacecrafts, Single event effects, total ionization dose, displacement damage.
Lecture 48:
Radiation charging of dielectric materials, physics ofradiation-Induced charging, radiation-induced bulk dischargesLecture 49:Modeling, Simulation, and Testing


Week 11:Radiation environment 3

Lecture 50:Coupling, victim, spacecraft radiation hardening
Lecture 51:
Test and evaluation, design guidelines, material selection, wiring and cable shields and their bonding
Lecture 52:Spacecraft radiation hardening, Radiation Hardness Assurance
Lecture 53:Design guidelines and mitigation techniques for the effects of radiation environment.

Risk assessment, reliability 1

Lecture 54:
Failures Caused by the Space Environment, a review of different space missions anomalies
Lecture 55:Risk assessment and management, general guidelines for risk assessment
Week 12:Risk assessment, reliability 2

Lecture 56:
Reliability and Quality Assurance, Parts reliability
Lecture 57:Satellite system availability

Mission planning, Spacecraft operations and safety

Lecture 58:Space mission drivers, different considerations of mission planning
Lecture 59:
Spacecraft operations: fault management systems
Lecture 60:
Autonomy in spacecraft operations, different approaches

Taught by

Prof. Soumyabrata Chakrabarty

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