MIT - 16.20
Fall, 2002
Unit 1
Introduction and Design Overview
Paul A. Lagace, Ph.D.
Professor of Aeronautics & Astronautics
and Engineering Systems
Paul A. Lagace
? 2001
MIT - 16.20
Fall, 2002
Need to study structural mechanics to design properly to prevent failure There is no doubt that any of the disciplines of Aeronautics and Astronautics can contribute to an accident
-engine failure -etc.
But, the vast majority of non-human induced accidents is due to structural (material) failure (ultimately). Purpose of 16.20
:
Provide you with the tools to properly
Design “Aerospace Structures
” to assure
“structural integrity”
(i.e., it doesn
’
t
fail)
Note
, 16.20 mainly oriented in past to aircraft structures because that is
where the main experience lies.
We will try to generalize and show
examples for space structures.
Paul A. Lagace
? 2001
Unit 1 -
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MIT - 16.20
Fall, 2002
Aeronautics and Astronautics deal with three major categories of structures:
1.
Aircraft (atmospheric vehicles)
2.
Launch vehicles
3.
Space structures (partially a civil engineering task?)
(
Note
:
Transatmospheric
vehicles can be
combinations of 1 and 2
…the Shuttle is!)
IMPORTANT
:
Many of the design considerations for these
three categories are different,
but
the
same
techniques
and
concepts
are
used
to
analyze
the
structures
(basically)
In fact, except for special design considerations, the techniques used for all structures are basically the same:
Paul A. Lagace
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MIT - 16.20
Fall, 2002
Possible considerations
Structure type
Buildings Ships Cars Space stations Airplanes
?
?
?
The difference is often in the degree of refinement of the structural analysis (generally more refined in A & A!)
null
We will teach basic techniques and concepts and use specific examples.
But, the technique may apply to another
structural type as well.
Example
:
(aircraft to space station)
Fuselage --> space station living habitat (pressurized cylinders)
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Fall, 2002
Overview of Structural Design Process
(Review from U.E.)
Purpose
:
Assure
“structural integrity”
while minimizing
cost
In aerospace structures, cost often means weight. Why?
Saving a pound of weight means more
- payload
(extra passengers, more satellites)
- fuel
(longer distance, longer duration via extended
station keeping)
? ? ?
Amount industries (civilian) are willing to pay to save a pound of weight:
Satellites
$10,000 - $20,000 (w/o servicing)
Transport Aircraft
$100 - $200
General Aircraft
$25
Automobile
~
$0.00
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MIT - 16.20
Fall, 2002
Sometimes willing to pay for performance
(military, FWC
…polar
orbit)
Factors in determining cost
?
Material cost
?
Waste amount
?
Manufacturing
?
Subassembly/assembly
?
Durability and maintenance
?
Useful life
An engineer must consider all these.
In 16.20 we will focus on
“structural integrity
” and methods to assess such.
Definition of
structural integrity
:
“Capability of a structure to carry out the operation for which it was designed.
”
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MIT - 16.20
Fall, 2002
Many aspects
?
Required loads
?
Required deformations
?
Corrosion resistance (e.g., no penetration on pressure vessels)
Many aspects to
“
failure
”
(we will discuss later)
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Fall, 2002
Design Process
5.
Determine capability of structure to carry loads
(of box 2) subject to design restrictions (of box 1)
4. 3.
size components
2.
environment to which structure is subjected
1.
2
1
Manufacturing & Maintenance
considered throughout
Determine internal stresses and deflections Layout structural arrangement, select materials, Determine applied loads and operating Design restrictions/specifications
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Fall, 2002
Iterative loops
?
Big loop
2
: May find there is no way to attain what was asked for
?
Loop
1
: Go through this all the time.
Get more and more
specific on design each time
- Use more refined techniques each time - Iterate to get most efficient structure
?
#1 usually given from
“above
”
?
#2 tells us what we need to consider
in
16.20
?
Learn to do #4 and #5
?
Use knowledge attained in 16.20 and by doing #4 a number of times to think about #3
Current use of
IPT
’s…customers
involved
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