1. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
DEPARTMENT OF AEROSPACE ENGG. UNIVERSITY INSTITUTE OF ENGINEERING CHANDIGARH UNIVERSITY, MOHALI
DEPARTMENT OF AEROSPACE ENGINEERING

2. AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
INTRODUCTION TO
AEROSPACE ENGINEERING
AST-105
Session : July- Dec 2018
Semester : I
J. S. Sandhu– E3856
Assistant Professor
Chandigarh University
DEPARTMENT OF AEROSPACE ENGINEERING

3. Introduction to flight principle & various systems in aircrafts
Introduction to Aerospace Engineering (AST-105)
UNIT-III
Introduction to flight principle & various systems in aircrafts
DEPARTMENT OF AEROSPACE ENGINEERING

4. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
COURSE OBJECTIVE
Course will prepare engineer about the basics of aircraft motion in three directions
Course will introduce students with current progress in aerospace engineering propulsion and electrical systems
DEPARTMENT OF AEROSPACE ENGINEERING

5. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
PRIMARY GOALS / LEARNING OBJECTIVE
The primary goal of this course is to recognize where the Aircrafts came from & the environment/ atmosphere they fly in.
The students will be able to understand the changes in aircraft performance with change in altitude. .
DEPARTMENT OF AEROSPACE ENGINEERING

6. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
COURSE PREREQUISITES
A first course in history of aviation is required. Additionally, students must have taken a course in thermodynamics, fluid mechanics.
DEPARTMENT OF AEROSPACE ENGINEERING

7. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
SYLLABUS
Introduction to history and growth of aerospace engineering, Indian space exploration and achievement,
Working principle of rockets and their propulsion system, solid fuel propulsion, liquid fuel propulsion etc, types of propellants used.
Introduction to types of rockets, missiles, satellite and reusable vehicles, International space station
DEPARTMENT OF AEROSPACE ENGINEERING

8. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
TOPIC COVERED
Introduction to history and growth of aerospace engineering, Indian space exploration and achievement,
Working principle of rockets and their propulsion system, solid fuel propulsion, liquid fuel propulsion etc, types of propellants used.
Introduction to types of rockets, missiles, satellite and reusable vehicles, International space station
DEPARTMENT OF AEROSPACE ENGINEERING

9. A Brief History of Space Exploration
Introduction to Aerospace Engineering (AST-105)
A Brief History of Space Exploration
DEPARTMENT OF AEROSPACE ENGINEERING

10. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
1942
In 1942 the German V2 was the first rocket to reach 100km from the Earth’s surface (the boundary of space). The rocket was designed by Wernher Von Braun, who later worked with NASA as the creator of the rockets that went to the moon.
DEPARTMENT OF AEROSPACE ENGINEERING

11. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
1947
In 1947, the first animals were launched into space. Fruit flies were used to study the effects of space travel on animals, and were chosen because they are more similar to humans than you might imagine! The flies travelled with a supply of corn to eat on the flight.
DEPARTMENT OF AEROSPACE ENGINEERING

12. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
1949
Albert II, was the first monkey in space. He was a Rhesus monkey, a type of monkey that originally comes from Asia. Albert went into space on June 14, 1949 in a specially adapted American V2 rocket, that flew to a height of 83 miles from earth.
DEPARTMENT OF AEROSPACE ENGINEERING

13. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
1957
On October 4, 1957, Russia launched the first satellite into space; Sputnik 1, and the space age had properly begun! Sputnik was the first satellite in orbit around the earth. Today there are over 500 working satellites in space. Sputnik means "Satellite" in Russian.
DEPARTMENT OF AEROSPACE ENGINEERING

14. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
1969
On July 20, 1969, Neil Armstrong, and then Buzz Aldrin, took "one small step" and became the first men on the moon. The first words said on the moon were "the Eagle has landed." Their spaceship, Apollo 11 worked perfectly, flying them 250,000 miles to the moon, and bringing them all the way back safely to earth.
DEPARTMENT OF AEROSPACE ENGINEERING

15. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
1957
In November 1957, the Russian space dog Laika became the first animal to orbit the earth. Laika travelled in a spacecraft known as Sputnik 2. Laika means "Barker" in Russian, and her mission helped scientists understand whether people could survive in space.
DEPARTMENT OF AEROSPACE ENGINEERING

16. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
1961
On April 12, 1961, Russian Cosmonaut Yuri Gagarin became the first man in space. Gagarin's spacecraft, Vostok 1, completed one orbit of the earth,
and landed about two hours after launch. Gagarin had to bail out and land using his parachute, because the Vostok 1 was designed to crash land!
DEPARTMENT OF AEROSPACE ENGINEERING

17. the airplane company famous for making the Jumbo Jet.
Introduction to Aerospace Engineering (AST-105)
From 1971, American astronauts on the fourth, fifth and sixth Apollo missions
enjoyed use of a moon car to explore the moon. Known as the “Lunar Rover,”
it was electric powered, and had a top speed of 8mph. It was designed and developed in only 17 months, by Boeing,
the airplane company famous for making the Jumbo Jet.
DEPARTMENT OF AEROSPACE ENGINEERING

18. 17,000 miles per hour. Six have been built.
Introduction to Aerospace Engineering (AST-105)
Until April 12, 1981 all spacecraft were designed to be used only once.
The Space Shuttle, was designed to be reused for up to 100 visits to space,
in an attempt to make space travel less expensive. With five hugely powerful rocket motors, it can fly at more than
17,000 miles per hour. Six have been built.
DEPARTMENT OF AEROSPACE ENGINEERING

19. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
On January 28, 1986, tragedy struck. The Challenger exploded shortly after launch, because of a fuel system failure. All seven astronauts on board were killed,
and all space shuttles were grounded for nearly three years. This shocking accident reminded the world of the dangers of space travel, and the incredible bravery of all astronauts.
DEPARTMENT OF AEROSPACE ENGINEERING

20. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
In 2000, the first permanent crew moved into the International Space Station,
where crews of astronauts have been living ever since. The ISS is a huge space station for research and space exploration that began construction in 1986 and was finished in 2010.
DEPARTMENT OF AEROSPACE ENGINEERING

21. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
On October:15, 2003, China sent its first man, Yang Liwei, into space. They succeed in becoming the third country ever to send a human into space.
DEPARTMENT OF AEROSPACE ENGINEERING

22. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Abbreviations Used in Aerospace Engg.
GCSLV: Guidance Controlled Satellite Launch Vehicle
VSSC: Vikram Sarabhai Space Centre at Thiruvanthapuram
SLV: Satellite Launch Vehicle
ASLV: Augmented Satellite Launch Vehicle
PSLV: Polar Satellite Launch Vehicle
DEPARTMENT OF AEROSPACE ENGINEERING

23. Indian Space Transportation System
Introduction to Aerospace Engineering (AST-105)
Indian Space Transportation System
Present Scenario and Future Directions
Rocket by Tippu Sultan
He used world’s first war rocket
against the British.
A long bamboo stick using 2 kg
gun powder as rocket & sword
as its weapon.
Each rocket weighed 3.5 kg and
traveled 1.5 km.
An outstanding performance.
Multiple rockets fired at the
same time pierced through the
British cavalry.
Tippu’s rocket is displayed at the Artillery Museum in Woolwich, London.
DEPARTMENT OF AEROSPACE ENGINEERING

24. Sounding Rockets of ISRO
Introduction to Aerospace Engineering (AST-105)
Sounding Rockets of ISRO
DEPARTMENT OF AEROSPACE ENGINEERING

25. ISRO Launch Vehicle Family
Introduction to Aerospace Engineering (AST-105)
ISRO Launch Vehicle Family
Aug 1979 /July 1980
May 1992
Oct 1994
Apr 2001
Middle 2010
GSLV Mk-III
SLV
ASLV
PSLV
GSLV
4(1)
4(2)
15(1)
5(1)
Height (m)
Lift-off wt(t)
Payload kg
Orbit LEO LEO POLAR GTO GTO
DEPARTMENT OF AEROSPACE ENGINEERING

26. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
DEPARTMENT OF AEROSPACE ENGINEERING

27. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
PSLV Configuration
6S9 + S139 + PL40 + HPS3 +L2.5
Gross weight : 294 T
Overall height: 44 m
Diameter : m
Heatshield: 3.2 m
Features :
4 stage vehicle
Multiple satellite launch capability
Multi orbit capability
Performance :
GTO : 1.2 T
SSPO : 1.7 T
DEPARTMENT OF AEROSPACE ENGINEERING

28. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Important elements of PSLV
1. Payload
2. Heat shield
3. Payload adapter
4. Equipment bay
5. Auxiliary payload
6. 4th stage tank
7. 4th stage engine
8. Antennae
9. Reaction thruster
10. Interstage 3/4
11. 3rd stage adapter
12. 3rd stage motor
13. Flex nozzle control
14. Interstage 2/3 U
. Interstage 2/3 L
16. 2nd stage tank
17. Interstage ½ U
18. 2nd stage retros
19. Ullage rocket (4)
20. Gimbal control
21. Interstage ½ L
22. 2nd stage engine
23. 1st stage retro
24. First stage motor
25. TVC injectant tank
26. Strap-on motor
27. TVC system
28. Core base shroud
29. Roll control engine
DEPARTMENT OF AEROSPACE ENGINEERING

29. PSLV C9: Spacecraft accommodation
Introduction to Aerospace Engineering (AST-105)
PSLV C9: Spacecraft accommodation
CARTOSAT – INDIA kg
NLS-5
IMS -1
INDIA kg
RUBIN 8
GERMANY
DEPARTMENT OF AEROSPACE ENGINEERING

30. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
GSLV Configuration
4L40 + S125 + L C12
LOW : 414 T
Diameter : m
Heatshield : 3.8 m
Features :
3 stage vehicle
Performance :
GTO : 2 t.
Performance growth
Potential : 2.5 t ( with indigenous Cryo stage
DEPARTMENT OF AEROSPACE ENGINEERING

31. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
DEPARTMENT OF AEROSPACE ENGINEERING

32. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
DEPARTMENT OF AEROSPACE ENGINEERING

33. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Indigenous Cryo Stage Development
Detailed qualifications tests have been carried out in engine in several ground tests.
Flight stage is getting ready and expected to fly by September 2009.
DEPARTMENT OF AEROSPACE ENGINEERING

34. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Chandrayaan 1
Launched by PSLV 11: 313 t
Date of Launch : 22nd Oct 2008
Chandrayaan 1
India kg
DEPARTMENT OF AEROSPACE ENGINEERING

35. DEPARTMENT OF AEROSPACE ENGINEERING
Chandrayaan 1 Mission Profile
Introduction to Aerospace Engineering (AST-105)
IO : 254x 22, km
EBN-1 : 301 x 37, km
EBN-2 : 336 x 74, km
EBN-3 : 348 x 1,65,016 km
EBN-4 : 460 x 2,66,509 km
EBN-5 : 977 x 3,80,513 km
LC : 508 x km
LBN-1 : 201 x 7502 km
LBN-2 : 183 x km
LBN-3 : 102 x km
LBN-4 : 102 x km
DEPARTMENT OF AEROSPACE ENGINEERING

36. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
DEPARTMENT OF AEROSPACE ENGINEERING

37. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
DEPARTMENT OF AEROSPACE ENGINEERING

38. Reusable Launch Vehicle using Air Breathing Propulsion
Introduction to Aerospace Engineering (AST-105)
Reusable Launch Vehicle using Air Breathing Propulsion
DEPARTMENT OF AEROSPACE ENGINEERING

39. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
DEPARTMENT OF AEROSPACE ENGINEERING

40. Spacecraft Classification
Introduction to Aerospace Engineering (AST-105)
Spacecraft Classification
Robotic spacecraft:
Are specially designed and constructed systems that can function in specific hostile environments. Their complexity and capabilities vary greatly and their purposes are diverse.
To make some sense of all these variables, this chapter arbitrarily designates eight broad classes of robotic spacecraft according to the missions the spacecraft are intended to perform: Flyby spacecraft 2. Orbiter spacecraft  3. Atmospheric spacecraft 4. Lander spacecraft 5. Rover spacecraft 6. Penetrator spacecraft 7. Observatory spacecraft 8. Communications spacecraft
DEPARTMENT OF AEROSPACE ENGINEERING

41. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Flyby Spacecraft
flyby spacecraft conducted the initial reconnaissance phase of solar system exploration.
They follow a continuous solar orbit or escape trajectory, never to be captured into a planetary orbit.
They must have the capability of using their instruments to observe targets they pass. Ideally, they can pan to compensate for the target's apparent motion in optical instruments' field of view
. They must downlink data to Earth, storing data onboard during the periods when their antennas are off Earthpoint.
They must be able to survive long periods of interplanetary cruise.
Flyby spacecraft may be designed to be stabilized in 3 axes using thrusters or reaction wheels or to spin continuously for stabilization.
Our prime example of the flyby spacecraft category is Voyager 2, which conducted encounters in the Jupiter, Saturn, Uranus, and Neptune systems. Click the Voyager image for details of the twin Voyager 1 and 2 spacecraft.
DEPARTMENT OF AEROSPACE ENGINEERING

42. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Orbiter Spacecraft
A spacecraft designed to travel to a distant planet and enter into orbit about it must carry with it a substantial propulsive capability to decelerate it at the right moment to achieve orbit insertion.
It has to be designed to live with the fact that solar occultations will occur, wherein the planet shadows the spacecraft, cutting off any solar panels' production of electrical power and subjecting the vehicle to extreme thermal variation.
Earth occultations will also occur, cutting off uplink and downlink communications with Earth. Orbiter spacecraft are carrying out the second phase of solar system exploration, following up the initial reconnaissance with in-depth study of each of the planets.
These include Magellan, Galileo, Mars Global Surveyor, and Cassini. Our prime example of the orbiter spacecraft category is Galileo which entered orbit about Jupiter in 1995 to carry out a highly successful study of the Jovian system
DEPARTMENT OF AEROSPACE ENGINEERING

43. Atmospheric Spacecraft
Introduction to Aerospace Engineering (AST-105)
Atmospheric Spacecraft
Atmospheric spacecraft:
Are designed for a relatively short mission to collect data about the atmosphere of a planet or satellite.
One typically has a limited complement of spacecraft subsystems. For example, an atmospheric spacecraft may have no need for propulsion subsystems or attitude and articulation control system subsystems at all.
It does require an electric power supply, which may simply be batteries, and telecommunications equipment for tracking and data relay.
Its scientific instruments may take direct measurements of an atmosphere's composition, temperature, pressure, density, cloud content and lightning.
DEPARTMENT OF AEROSPACE ENGINEERING

44. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Lander Spacecraft
Are designed to reach the surface of a planet and survive long enough to telemeter data back to Earth.
Examples have been the highly successful Soviet Venera landers which survived the harsh conditions on Venus while carrying out chemical composition analyses of the rocks and relaying color images, JPL's Viking landers at Mars, and the Surveyor series of landers at Earth's moon, which carried out similar experiments.
The Mars Pathfinder project, which landed on Mars on July 4, 1997, and deployed a rover, was intended to be the first in a series of landers on the surface of Mars at widely distributed locations to study the planet's atmosphere, interior, and soil.
A system of actively-cooled, long-lived Venus landers designed for seismology investigations, is being envisioned for a possible future mission.
DEPARTMENT OF AEROSPACE ENGINEERING

45. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Penetrator Spacecraft
Surface penetrators:
Have been designed for entering the surface of a body, such as a comet, surviving an impact of hundreds of Gs, measuring, and telemetering the properties of the penetrated surface.
As of November 2000, no Penetrator spacecraft have been successfully operated. Penetrator data would typically be telemetered to an orbiter craft for re- transmission to Earth.
The Comet Rendezvous / Asteroid Flyby (CRAF) mission included a cometary penetrator, but the mission was cancelled in 1992 due to budget constraints. Our prime example of a penetrator spacecraft is the twin Deep Space 2 penetrators which piggybacked to Mars aboard the Mars Polar Lander and were to slam into Martian soil December 3, 1999.
They were never heard from
DEPARTMENT OF AEROSPACE ENGINEERING

46. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Rover Spacecraft
Electrically-powered rover spacecraft :
Are being designed and tested by JPL as part of Mars exploration effort.
The Mars Pathfinder project included a small, highly successful mobile system referred to as a micro-rover by the name of Sojourner. Mars rovers are also being developed by Russia with a measure of support from The Planetary Society.
Rover craft need to be semi-autonomous. They are steerable from Earth. Their purposes range from taking images and soil analyses to collecting samples for return to Earth. Our prime example of a rover spacecraft is of course the famous show Sojourner.
DEPARTMENT OF AEROSPACE ENGINEERING

47. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Observatory Spacecraft
Does not travel to a destination to explore it. Instead, it occupies an Earth orbit or a solar orbit from where it can observe distant targets free of the obscuring and blurring effects of Earth's atmosphere. NASA's Great Observatories program studies the universe at wavelengths from visible light to gamma- rays.
The program includes four Observatory Spacecraft: the familiar,
Hubble Space Telescope (HST),
The Chandra X-Ray Observatory (CXO -- previously known as AXAF),
The Compton Gamma Ray Observatory (GRO),
And the Space Infrared Telescope Facility (SIRTF).
DEPARTMENT OF AEROSPACE ENGINEERING

48. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Communications Spacecraft
Are abundant in Earth orbit, but they are largely incidental to JPL's missions. The Deep Space Network's Ground Communications Facility does make use of Earth-orbiting communications spacecraft to transfer data among its sites in Spain, Australia, California, and JPL. In the future, communications spacecraft may be deployed at Mars, Venus, or other planets to communicate with orbiters, rovers, penetrators, and atmospheric spacecraft operating in their vicinity.
Their purpose would be to augment the Deep Space Network's capabilities to communicate with the resident spacecraft
DEPARTMENT OF AEROSPACE ENGINEERING

49. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Rocket Powered Airplanes
Uses a rocket engine for propulsion
Has higher speeds
Propels only for a short period of time
Unusual launch configurations
From another plane
Vertically – nose in the air and tail to the ground
DEPARTMENT OF AEROSPACE ENGINEERING

50. Rocket Assisted Take Off
Introduction to Aerospace Engineering (AST-105)
Rocket Assisted Take Off
Also known as a rocket plane, it is an aircraft that uses a rocket for propulsion, sometimes in addition to air- breathing jet engines (known as Jet Assisted Take Off). They can fly at much faster speeds than a jet aircraft of similar size, but only work for a few minutes, followed by a glide. Because they are powered by a rocket which does not need oxygen from the atmosphere, they are good for very high altitude flight. They also accelerate faster, and therefore have shorter takeoffs.
DEPARTMENT OF AEROSPACE ENGINEERING

51. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Rocket Propulsion
Newton’s 3rd Law:
For every action there is an equal and opposite reaction.
Rocket engines generate thrust by putting a gas under pressure.
The gas escaping the rocket is called exhaust.
As the rocket pushes the exhaust backward, the exhaust pushes the rocket forward.
Engine pushes itself forward or upward by producing thrust
A rocket engine uses only propellant carried within it.
It carries
A rocket can operate in outer space, where there is almost no air
DEPARTMENT OF AEROSPACE ENGINEERING

52. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Rocket Propellant
Solid-Fuel Rockets
Burn a solid material called the grain
Engineers design grains with a hollow core
Propellant burns from the core outward
Unburned propellant shields the engine casing from the heat of combustion
DEPARTMENT OF AEROSPACE ENGINEERING

53. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Rocket Propellant
Solid-Fuel Rockets
Hollow Core
Solid Fuel
DEPARTMENT OF AEROSPACE ENGINEERING

54. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Rocket Propellant
Liquid-Fuel Rocket
Carries fuel and oxidizer in separate tanks
Fuel circulates through cooling jacket before entering combustion chamber
Circulation preheats the fuel for combustion and helps cool the rocket
DEPARTMENT OF AEROSPACE ENGINEERING

55. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Rocket Propellant
Ion (Electric)
Coils are heated to change a fuel, such as xenon, into a vapor
Hot platinum or tungsten ionization grid changes the flowing vapor into a stream of electrically charged particles called ions
DEPARTMENT OF AEROSPACE ENGINEERING

56. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Rocket Propellant
Nuclear
Uses heat from a nuclear reactor to change a liquid fuel into a gas
Some of the fuel, heated by the nozzle of the rocket, flows through the turbine
Turbine drives the fuel pump
DEPARTMENT OF AEROSPACE ENGINEERING

57. RECOMMENDED BOOKS Introduction to Aerospace Engineering (AST-105)
Sr .No
Title
Author
Editio n
Year
Publisher Name 1
Rocket propulsion and Space Flight Dynamics
J.W. Cornelisse
1979
Pitman 2
Introduction to flight
John D Anderson 8
2016
MgGraw-Hill,
DEPARTMENT OF AEROSPACE ENGINEERING

58. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
LEARNING OUTCOMES
To be able to state the principle of working of aircraft propulsion (quiz, self-assessment)
To be able to understand the history of Indian space aviation. (quiz, homework, self-assessment)
DEPARTMENT OF AEROSPACE ENGINEERING

59. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Course Outcome
The student should be able to understand the space history, various launch vehicles and their uses. They will also learn about the rocket propulsion system of missiles and space launch vehicles.
DEPARTMENT OF AEROSPACE ENGINEERING

60. DEPARTMENT OF AEROSPACE ENGINEERING
Introduction to Aerospace Engineering (AST-105)
Reference Books
1. A C Kermode, Flight without formulae, McGraw Hill, 1997
DEPARTMENT OF AEROSPACE ENGINEERING