Structure Design HW #2

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1 Structure Design HW #2 祝祝祝 12/12/2008

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Structure Design HW #2. 祝飛鴻 12/12/2008. Concept of Process. “Process” is a step-by-step planning in resolution of problems with identified inter-relation and sequence between the steps. When facing problems, the common mistake is to - PowerPoint PPT Presentation

Transcript of Structure Design HW #2

Page 1: Structure Design HW #2

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Structure Design HW #2

祝飛鴻12/12/2008

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“Process” is a step-by-step planning in resolution of

problems with identified inter-relation and sequence

between the steps.

When facing problems, the common mistake is to

immediately jump into the execution details without

an overall, from beginning to end, problem solving

“process”.

Depends on the situation, the “process” may not need

to be in detail to start with. The “process” can be

modified or enhanced during execution.

Concept of Process

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Without a proper pre-defined “process”, most likely,

it will lead to lengthy iteration in solving problems.

The “process” can also be used to align all the involved

parties to work with the same pace. This is extremely

important for large scale projects, e.g. satellite design.

Concept of Process

“Process” can be presented as flow

chart with waterfall concept, i.e. top

down from coarse to detail.

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Following chart provide a typical process related to the spacecraft structure design. It is not intended to be a standard solution, but rather to be a reference information for the homework problem.

Structure Design HW #2

Q: Generate a detail flow chart for spacecraft structure

design, from requirements to verification.

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SpacecraftStructure Design

Requirements &

Constraints

Design &

Analysis

Verification &

Validation

Waterfall Structure

Mission Driven

LV Driven

System DrivenConfiguration Design

Stress Analysis

Dynamic Analysis

Special Analysis

Verification Plan

Test Plan

Test Procedures

Level 1

Level 2

Level 3

Lift-off wt

Fairing Size

Launch Loads

Acoustic Loads

Random Loads Quasi-static Loads

Shock Loads

Level 4

Level 5

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Mission Orbit Target wt & Size

Conceptual Design

Candidate LV

Wt Limitation Fairing SizeLaunch Loads

Component Selection

Wt & Size FOV Orientation

System RequirementsMission Requirements

Configuration Design

Finite Element ModelStress Analysis

Dynamic Analysis

Coupled Loads Results

Design Verification

Environmental Test

Min Freq Reqt

Test Plan & Procedures

Verification Plan

Material Selection

Preliminary Sizing