
Explore spacecraft propulsion concepts, from chemical and electrical propulsion to auxiliary systems and interplanetary trajectories, along with rendezvous and docking stages.
Explore spacecraft subsystems and propulsion types, differentiate primary and auxiliary propulsion, and examine how propulsion relates to attitude control and torque calculations.
Explore the two-body problem to model spacecraft motion around a central body, using Keplerian motion, orbital energy, and key orbital elements while noting assumptions and limitations.
Explore the parameters of elliptical orbits, including foci, apse line, semi-major axis a, rp and ra, and learn key equations for velocity, angular momentum, and time since periapsis.
Explore parabolic and hyperbolic orbits, e=1 and e>1, escape velocity and hyperbolic excess speed v∞, and the energy parameter C3 for interplanetary missions.
Evaluate delta-V and time of flight for transferring between geocentric elliptical orbits, comparing Hohmann and bielliptic paths, and estimate propellant mass from ΔV with Ve = 3500 m/s.
Explore phasing maneuvers to rendezvous in the same orbit by adjusting speed to change orbital period, and calculate the required total delta-V to meet the target for berthing or docking.
Explore plane change maneuvers and combined maneuvers for inter-orbit transfers, detailing apse-line misalignment, inclination changes, and three delta-v scenarios to compare efficiency.
Explore reaching lunar orbit through the circular restricted three-body problem, from low Earth orbit to the Moon. Detail delta-V, time of flight, and rendezvous considerations.
Survey visiting vehicles to the International Space Station, including Soyuz for crew, Progress and ATV for cargo, and Dragon and Starliner under NASA's commercial crew and cargo program.
Explore chemical propulsion with cold gas and mono-propellant systems for small spacecraft, detailing propellant tanks, regulators, and electronic controls, and compare nitrogen and hydrogen gas options, performance, and mission applications.
Explore blowdown systems for mono propellent propulsion, where a gas pressure drives the propellent and thrust decays as pressure falls, affecting mission margins and control.
Examine electrical propulsion, including electrostatic and electromagnetic thrusters, how propellant is accelerated, and how onboard power from solar or nuclear sources limits performance and efficiency for long-duration spaceflight.
Explore ISS visiting vehicles, including SpaceX Dragon for crew and cargo, European and Japanese ATVs, and Russian Progress, with refueling, reboost, and diverse propulsion systems.
The course helps to grasp the principles of spacecraft propulsion technologies in different space regions, orbital mechanics to estimate the velocity change requirement for phase change, plane change and station keeping. It covers how to dock or berth to another spacecraft in space and interplanetary trajectories.
It gives emphasis on understanding the concepts in a systematic manner and its application with worked examples of real time data. It helps to understand and analyze the specifications of spacecraft propulsion system like Dragon, Orion and Soyuz. Also, impart knowledge to estimate required propellant to meet a particular space mission.
The course in detail covers major concepts spacecraft propulsion technologies. The working and characteristics of chemical propulsion systems, cold gas, mono and bi-propellant are explained and space missions used these systems are described. The principles and working of electrical propulsion systems like electrothermal, electrostatic, electromagnetic are described. The course explains the fluid flow and energy conversion pattern in electrical propulsion units. The concepts of advanced space propulsion systems like solar and nuclear are discussed. The interplanetary trajectories, departure, transfer and arrival are explained in detail. The advantage of planet’s gravity in adding the required velocity change in interplanetary travel of spacecraft is explained. It discusses NASA’s ARTEMIS program and major problems of human Mar’s mission.