MARC details
| 000 -LEADER |
|---|
| fixed length control field |
14626cam a2200397 i 4500 |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
|---|
| control field |
20221102172110.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
|---|
| fixed length control field |
110626s2012 gw a b 001 0 eng d |
| 011 ## - LINKING LIBRARY OF CONGRESS CONTROL NUMBER [OBSOLETE] |
|---|
| Local cataloguing issues note |
BIB MATCHES WORLDCAT |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
|---|
| International Standard Book Number |
3642225365 |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
|---|
| International Standard Book Number |
9783642225369 |
| 035 ## - SYSTEM CONTROL NUMBER |
|---|
| System control number |
(ATU)b12489621 |
| 035 ## - SYSTEM CONTROL NUMBER |
|---|
| System control number |
(OCoLC)733249494 |
| 040 ## - CATALOGING SOURCE |
|---|
| Original cataloging agency |
BTCTA |
| Language of cataloging |
eng |
| Description conventions |
rda |
| Transcribing agency |
BTCTA |
| Modifying agency |
UKMGB |
| -- |
YDXCP |
| -- |
TJC |
| -- |
ATU |
| 050 #4 - LIBRARY OF CONGRESS CALL NUMBER |
|---|
| Classification number |
TL545 |
| Item number |
.A43 2012 |
| 082 04 - DEWEY DECIMAL CLASSIFICATION NUMBER |
|---|
| Classification number |
629.1 |
| Edition number |
23 |
| 100 1# - MAIN ENTRY--PERSONAL NAME |
|---|
| Personal name |
Alber, Irwin E., |
| Relator term |
author. |
| 9 (RLIN) |
1094531 |
| 245 10 - TITLE STATEMENT |
|---|
| Title |
Aerospace engineering on the back of an envelope / |
| Statement of responsibility, etc. |
Irwin E. Alber. |
| 264 #1 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE |
|---|
| Place of production, publication, distribution, manufacture |
Heidelberg : |
| Name of producer, publisher, distributor, manufacturer |
Springer ; |
| Place of production, publication, distribution, manufacture |
Chichester, UK : |
| Name of producer, publisher, distributor, manufacturer |
Published in association with Praxis Publishing, |
| Date of production, publication, distribution, manufacture, or copyright notice |
2012. |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Extent |
xix, 326 pages : |
| Other physical details |
illustrations ; |
| Dimensions |
25 cm. |
| 336 ## - CONTENT TYPE |
|---|
| Content type term |
text |
| Content type code |
txt |
| Source |
rdacontent |
| 337 ## - MEDIA TYPE |
|---|
| Media type term |
unmediated |
| Media type code |
n |
| Source |
rdamedia |
| 338 ## - CARRIER TYPE |
|---|
| Carrier type term |
volume |
| Carrier type code |
nc |
| Source |
rdacarrier |
| 490 1# - SERIES STATEMENT |
|---|
| Series statement |
Springer-Praxis books in astronautical engineering |
| 504 ## - BIBLIOGRAPHY, ETC. NOTE |
|---|
| Bibliography, etc. note |
Includes bibliographical references and index. |
| 505 0# - FORMATTED CONTENTS NOTE |
|---|
| Formatted contents note |
1. Introduction -- 2. Design of a high school science-fair electro-mechanical robot -- 3. Estimating Shuttle launch, orbit, and payload magnitudes -- 4. Columbia Shuttle accident analysis with Back-of-the-Envelope methods -- 5. Estimating the Orbiter reentry trajectory and the associated peak heating rates -- 6. Estimating the dimensions and performance of the Hubble Space Telescope -- -- |
| 505 00 - FORMATTED CONTENTS NOTE |
|---|
| Miscellaneous information |
1. |
| Title |
Introduction -- |
| Miscellaneous information |
1.1. |
| Title |
Why Back-of-the-Envelope engineering? -- |
| Miscellaneous information |
1.1.1. |
| Title |
Back-of-the-Envelope engineering; an important adaptation and survival skill for students and practicing engineers -- |
| Miscellaneous information |
1.1.2. |
| Title |
Design of a high school science fair electro-mechanical robot -- |
| Miscellaneous information |
1.1.3. |
| Title |
Design of a new commercial rocket launch vehicle for a senior engineering student's design project -- |
| Miscellaneous information |
1.1.4. |
| Title |
Preliminary design of a new telescope system by an engineer transferred to a new optical project -- |
| Miscellaneous information |
1.1.5. |
| Title |
Examining the principles and ideas behind Back-of-the- Envelope estimation -- |
| Miscellaneous information |
1.2. |
| Title |
What is a Back-of-the-Envelope engineering estimate? -- |
| Miscellaneous information |
1.2.1. |
| Title |
Tradeoffbetween complexity and accuracy -- |
| Miscellaneous information |
1.2.2. |
| Title |
Back-of-the-Envelope reasoning -- |
| Miscellaneous information |
1.2.3. |
| Title |
Fermi problems -- |
| Miscellaneous information |
1.2.4. |
| Title |
An engineering Fermi problem -- |
| Miscellaneous information |
1.3. |
| Title |
General guidelines for building a good engineering model -- |
| Miscellaneous information |
1.3.1. |
| Title |
Step by step towards estimation -- |
| Miscellaneous information |
1.3.2. |
| Title |
Quick-Fire estimates -- |
| Miscellaneous information |
1.4. |
| Title |
Quick-Fire estimate of cargo mass delivered to orbit by the Space Shuttle -- |
| Miscellaneous information |
1.4.1. |
| Title |
Cargo mass problem definition -- |
| Miscellaneous information |
1.4.2. |
| Title |
Level-0 estimate: the empirical ''rule of thumb'' model -- |
| Miscellaneous information |
1.4.3. |
| Title |
Level-1 estimate: cargo mass using a single stage mathematical model based on the ideal rocket velocity equation -- |
| Miscellaneous information |
1.4.4. |
| Title |
Level-2 estimate: cargo mass using a two stage vehicle model based on the ideal rocket velocity equation -- |
| Miscellaneous information |
1.4.5. |
| Title |
Level-3 estimate: cargo mass delivered by a two stage vehicle; based on a revised estimate for second stage structural mass fraction -- |
| Miscellaneous information |
1.4.6. |
| Title |
Impact of added knowledge and degree of model complexity -- |
| Miscellaneous information |
1.4.7. |
| Title |
Moving from the Shuttle to the Hubble Space Telescope -- |
| Miscellaneous information |
1.5. |
| Title |
Estimating the size of the optical system for the Hubble Space Telescope -- |
| Miscellaneous information |
1.5.1. |
| Title |
System requirements for the HST -- |
| Miscellaneous information |
1.5.2. |
| Title |
Shuttle constraint on HST size -- |
| Miscellaneous information |
1.5.3. |
| Title |
Estimating the length of the HST optical package -- |
| Miscellaneous information |
1.6. |
| Title |
Concluding remarks -- |
| Miscellaneous information |
1.7. |
| Title |
Outline of this book -- |
| Miscellaneous information |
1.8. |
| Title |
References -- |
| Miscellaneous information |
2. |
| Title |
Design of a high school science-fair electro-mechanical robot -- |
| Miscellaneous information |
2.1. |
| Title |
The Robot-Kicker Science Fair Project -- |
| Miscellaneous information |
2.2. |
| Title |
Back-of-the-Envelope model and analysis for a solenoid kicking device -- |
| Miscellaneous information |
2.2.1. |
| Title |
Defining basic dimensions and required soccer ball velocity -- |
| Miscellaneous information |
2.2.2. |
| Title |
Setting up a Bot Emodel for the solenoid kicking soccer ball problem -- |
| Miscellaneous information |
2.2.3. |
| Title |
Model for solenoid kicker work and force -- |
| Miscellaneous information |
2.2.4. |
| Title |
Final design requirements for linear-actuator solenoid and supporting electrical system -- |
| Miscellaneous information |
2.3. |
| Title |
Appendix: Modeling of the temperature rise produced by ohmic heating from single or multiple solenoid-actuator kicks -- |
| Miscellaneous information |
2.3.1. |
| Title |
Quick-Fire problem approach -- |
| Miscellaneous information |
2.3.2. |
| Title |
Problem definition and sketch -- |
| Miscellaneous information |
2.3.3. |
| Title |
The baseline mathematical model -- |
| Miscellaneous information |
2.3.4. |
| Title |
Physical parameters and data -- |
| Miscellaneous information |
2.3.5. |
| Title |
Numerical results -- |
| Miscellaneous information |
2.3.6. |
| Title |
Interpretation of results -- |
| Miscellaneous information |
2.4. |
| Title |
References -- |
| Miscellaneous information |
3. |
| Title |
Estimating Shuttle launch, orbit, and payload magnitudes -- |
| Miscellaneous information |
3.1. |
| Title |
Introduction -- |
| Miscellaneous information |
3.1.1. |
| Title |
Early Space Shuttle goals and the design phase -- |
| Miscellaneous information |
3.1.2. |
| Title |
The Shuttle testing philosophy and the need for modeling -- |
| Miscellaneous information |
3.1.3. |
| Title |
Back-of-the-Envelope analysis of Shuttle launch, orbit, and payload magnitudes -- |
| Miscellaneous information |
3.2. |
| Title |
Shuttle launch, orbit, and reentry basics -- |
| Miscellaneous information |
3.2.1. |
| Title |
The liftoffto orbit sequence -- |
| Miscellaneous information |
3.2.2. |
| Title |
Reentry -- |
| Miscellaneous information |
3.3. |
| Title |
Inventory of the Shuttle's mass and thrust as input to the calculation of burnout velocity -- |
| Miscellaneous information |
3.3.1. |
| Title |
Burnout velocity -- |
| Miscellaneous information |
3.3.2. |
| Title |
The velocity budget -- |
| Miscellaneous information |
3.3.3. |
| Title |
Mass inventory -- |
| Miscellaneous information |
3.3.4. |
| Title |
Thrust and specific impulse inventory -- |
| Miscellaneous information |
3.4. |
| Title |
Mass fraction rules of thumb -- |
| Miscellaneous information |
3.5. |
| Title |
Quick-Fire modeling of the takeoffmass components and takeoffthrust using SMAD rules of thumb -- |
| Miscellaneous information |
3.5.1. |
| Title |
Quick-Fire problem approach -- |
| Miscellaneous information |
3.5.2. |
| Title |
Problem definition and sketch -- |
| Miscellaneous information |
3.5.3. |
| Title |
Mathematical/''Rule of Thumb'' empirical models -- |
| Miscellaneous information |
3.5.4. |
| Title |
Physical parameters and data -- |
| Miscellaneous information |
3.5.5. |
| Title |
Numerical calculation of total takeoffmass, cargo bay mass, and total takeoffthrust -- |
| Miscellaneous information |
3.5.6. |
| Title |
Interpretation of the Quick-Fire results -- |
| Miscellaneous information |
3.5.7. |
| Title |
From Quick-Fire estimates to Shuttle solutions using more accurate inputs -- |
| Miscellaneous information |
3.6. |
| Title |
Ideal velocity change Dv for each stage of an ideal rocket system -- |
| Miscellaneous information |
3.6.1. |
| Title |
Propellant mass versus time -- |
| Miscellaneous information |
3.6.2. |
| Title |
Time varying velocity change -- |
| Miscellaneous information |
3.6.3. |
| Title |
Effective burnout time and average flow rate -- |
| Miscellaneous information |
3.6.4. |
| Title |
Ideal altitude or height for each rocket stage -- |
| Miscellaneous information |
3.7. |
| Title |
Dvideal estimate for Shuttle first stage, without gravity loss -- |
| Miscellaneous information |
3.7.1. |
| Title |
Estimate of SSME propellant mass burned during first stage -- |
| Miscellaneous information |
3.7.2. |
| Title |
First stage mass ratio and average effective exhaust velocity -- |
| Miscellaneous information |
3.7.3. |
| Title |
Average specific impulse for the ''parallel'' (solidþliquid) first stage burn -- |
| Miscellaneous information |
3.7.4. |
| Title |
Dvideal estimate for Shuttle first stage -- |
| Miscellaneous information |
3.7.5. |
| Title |
Dvideal and altitude as functions of time, for the Shuttle first stage -- |
| Miscellaneous information |
3.8. |
| Title |
The effect of gravity on velocity during first stage flight -- |
| Miscellaneous information |
3.8.1. |
| Title |
Modeling the effects of gravity for a curved flight trajectory -- |
| Miscellaneous information |
3.8.2. |
| Title |
Time-varying pitch angle model -- |
| Miscellaneous information |
3.8.3. |
| Title |
Effect of gravity on rocket velocity during first stage flight -- |
| Miscellaneous information |
3.8.4. |
| Title |
Effect of gravity on rocket height during first stage flight -- |
| Miscellaneous information |
3.8.5. |
| Title |
Comparing model velocity and altitude with Shuttle data -- |
| Miscellaneous information |
3.8.6. |
| Title |
Gravity loss magnitudes for previously flown launch systems -- |
| Miscellaneous information |
3.8.7. |
| Title |
Model velocity, with gravity loss, compared with flight data -- |
| Miscellaneous information |
3.8.8. |
| Title |
Calculation of gravity-loss corrected velocity at first stage burnout -- |
| Miscellaneous information |
3.9. |
| Title |
The effect of drag on Shuttle velocity at end of first stage flight -- |
| Miscellaneous information |
3.9.1. |
| Title |
Modeling the effects of drag in the equation of motion -- |
| Miscellaneous information |
3.9.2. |
| Title |
Estimating first stage drag loss -- |
| Miscellaneous information |
3.9.3. |
| Title |
Final drag and gravity-corrected velocity at first stage burnout; key elements of the overall ''velocity budget'' for the first stage -- |
| Miscellaneous information |
3.10. |
| Title |
Calculation of second stage velocities and gravity losses -- |
| Miscellaneous information |
3.10.1. |
| Title |
Pitch and gravity loss modeling for the second stage flight period -- |
| Miscellaneous information |
3.10.2. |
| Title |
Time-varying gravity loss solution, region 2a -- |
| Miscellaneous information |
3.10.3. |
| Title |
Time-varying velocity solution, region 2b -- |
| Miscellaneous information |
3.10.4. |
| Title |
Combined velocity solution for regions1, 2a, and 2b and v(MECO) -- |
| Miscellaneous information |
3.11. |
| Title |
Summary of predicted Dv budget for the Shuttle -- |
| Miscellaneous information |
3.12. |
| Title |
Comparison of Back-of-the-Envelope modeled Shuttle velocity and altitude as a function of time to NASA's numerical prediction for all stages -- |
| Miscellaneous information |
3.12.1. |
| Title |
Comparison of model velocity with NASA's numerical prediction -- |
| Miscellaneous information |
3.12.2. |
| Title |
Comparison of model altitude with NASA's numerical prediction -- |
| Miscellaneous information |
3.12.3. |
| Title |
Modeled altitude sensitivity to pitch time scale -- |
| Miscellaneous information |
3.13. |
| Title |
Estimating mission orbital velocity requirements for the Shuttle -- |
| Miscellaneous information |
3.13.1. |
| Title |
Part1: circular orbital velocity -- |
| Miscellaneous information |
3.13.2. |
| Title |
Part2: elliptical orbits and the Hohmann transfer Dv's -- |
| Miscellaneous information |
3.13.3. |
| Title |
Numerical values for transfer orbit Dv's -- |
| Miscellaneous information |
3.13.4. |
| Title |
Time of flight for a Hohmann transfer -- |
| Miscellaneous information |
3.13.5. |
| Title |
Direct insertion to a final orbital altitude (without using a parking orbit) -- |
| Miscellaneous information |
3.14. |
| Title |
A Back-of-the-Envelope model to determine Shuttle payload as a function of orbit altitude -- |
| Miscellaneous information |
3.14.1. |
| Title |
Analytic model for payload as a function of orbital altitude -- |
| Miscellaneous information |
3.14.2. |
| Title |
Approximate linearized solution for payload -- |
| Miscellaneous information |
3.14.3. |
| Title |
Reduction in useful cargo mass due to increases in OMS propellant mass -- |
| Miscellaneous information |
3.14.4. |
| Title |
OMS models for correcting cargo or payload mass -- |
| Miscellaneous information |
3.14.5. |
| Title |
Model for rate of change of ''useful cargo'' with altitude -- |
| Miscellaneous information |
3.14.6. |
| Title |
Approximate analytic model for useful cargo -- |
| Miscellaneous information |
3.14.7. |
| Title |
Modeling missions to the International Space Station -- |
| Miscellaneous information |
3.15. |
| Title |
Tabulated summary of Back-of-the-Envelope equations and numerical results -- |
| Miscellaneous information |
3.16. |
| Title |
References -- |
| 505 00 - FORMATTED CONTENTS NOTE |
|---|
| Miscellaneous information |
4. |
| Title |
Columbia Shuttle accident analysis with Back-of-the-Envelope methods -- |
| Miscellaneous information |
4.1. |
| Title |
The Columbia accident and Back-of-the-Envelope analysis -- |
| Miscellaneous information |
4.1.1. |
| Title |
Bot Emodeling goals for the Columbia accident -- |
| Miscellaneous information |
4.1.2. |
| Title |
Quick estimation vs accurate estimation -- |
| Miscellaneous information |
4.2. |
| Title |
Quick-Fire modeling of the impact velocity of a piece of foam striking the Orbiter wing -- |
| Miscellaneous information |
4.2.1. |
| Title |
Interpretation of Quick-Fire results -- |
| Miscellaneous information |
4.2.2. |
| Title |
The bridge to more accurate Bot Eresults -- |
| Miscellaneous information |
4.3. |
| Title |
Modeling the impact velocity of a piece of foam debris relative to the Orbiter wing; estimations beyond the Quick-Fire time results -- |
| Miscellaneous information |
4.3.1. |
| Title |
Looking at the collision from an earth-fixed or moving Shuttle coordinate system -- |
| Miscellaneous information |
4.3.2. |
| Title |
The constant drag approximation -- |
| Miscellaneous information |
4.3.3. |
| Title |
Analytically solving for the impact velocity and mass, given the time to impact -- |
| Miscellaneous information |
4.3.4. |
| Title |
Summary of results for constant acceleration model compared to data -- |
| Miscellaneous information |
4.3.5. |
| Title |
The non-constant acceleration solution -- |
| Miscellaneous information |
4.3.6. |
| Title |
An estimate of impact velocity and particle mass, taking the time to impact as given (the ''inverse'' problem) -- |
| Miscellaneous information |
4.3.7. |
| Title |
Comparing Osheroff 's ''inverse'' calculations to our ''direct'' estimate results -- |
| Miscellaneous information |
4.3.8. |
| Title |
Concluding thoughts on the impact velocity estimate -- |
| Miscellaneous information |
4.4. |
| Title |
Modeling the impact pressure and load caused by impact of foam debris with an RCC wing panel -- |
| Miscellaneous information |
4.4.1. |
| Title |
The impact load -- |
| Miscellaneous information |
4.4.2. |
| Title |
Impact overview -- |
| Miscellaneous information |
4.4.3. |
| Title |
Impact load mathematical modeling -- |
| Miscellaneous information |
4.4.4. |
| Title |
Elastic model for the impact stress -- |
| Miscellaneous information |
4.4.5. |
| Title |
Elastic-plastic impact of a one-dimensional rod against a rigid-wall -- |
| Miscellaneous information |
4.4.6. |
| Title |
The elastic-plastic model -- |
| Miscellaneous information |
4.4.7. |
| Title |
Numerical results and plotted trends -- |
| Miscellaneous information |
4.4.8. |
| Title |
Impact area estimate -- |
| Miscellaneous information |
4.4.9. |
| Title |
Load estimate -- |
| Miscellaneous information |
4.4.10. |
| Title |
Impact loading time scale (Bot E) -- |
| Miscellaneous information |
4.4.11. |
| Title |
Loading time histories, numerical simulations -- |
| Miscellaneous information |
4.5. |
| Title |
Develop a Back-of-the-Envelope engineering stress equation for the maximum stress in the RCC panel face for a given panel load -- |
| Miscellaneous information |
4.5.1. |
| Title |
Bot Epanel stress model -- |
| Miscellaneous information |
4.5.2. |
| Title |
Estimates for the allowable maximum stress or critical load parameters for failure -- |
| Miscellaneous information |
4.5.3. |
| Title |
Final comments on the prediction of possible wing damage or failure -- |
| Miscellaneous information |
4.6. |
| Title |
Summary of results for Sections 4.2, 4.3, and 4.4 -- |
| Miscellaneous information |
4.7. |
| Title |
References -- |
| Miscellaneous information |
5. |
| Title |
Estimating the Orbiter reentry trajectory and the associated peak heating rates -- |
| Miscellaneous information |
5.1. |
| Title |
Introduction -- |
| Miscellaneous information |
5.2. |
| Title |
The deorbit and reentry sequence -- |
| Miscellaneous information |
5.3. |
| Title |
Using Quick-Fire methods to crudely estimate peak heating rate and total heat loads from the initial Orbiter kinetic energy -- |
| Miscellaneous information |
5.3.1. |
| Title |
Quick-Fire problem definition and sketch -- |
| Miscellaneous information |
5.3.2. |
| Title |
The Quick-Fire baseline mathematical model, initial results, and interpretation -- |
| Miscellaneous information |
5.4. |
| Title |
Alook at heat flux prediction levels based on an analytical model for blunt-body heating -- |
| Miscellaneous information |
5.4.1. |
| Title |
Numerical estimates of Stanton number using the Sutton- Graves constant -- |
| Miscellaneous information |
5.5. |
| Title |
Simple flight trajectory model -- |
| Miscellaneous information |
5.5.1. |
| Title |
Asimple Bot Emodel for the initial entry period; the entry solution -- |
| Miscellaneous information |
5.5.2. |
| Title |
The equilibrium glide model -- |
| Miscellaneous information |
5.6. |
| Title |
Calculating heat transfer rates in the peak heating region -- |
| Miscellaneous information |
5.6.1. |
| Title |
Selecting the nose radius -- |
| Miscellaneous information |
5.6.2. |
| Title |
Comparing the model maximum rate of heat transfer, q_wmax , with data -- |
| Miscellaneous information |
5.6.3. |
| Title |
Model estimate for nose radiation equilibrium temperature, Tmax -- |
| Miscellaneous information |
5.6.4. |
| Title |
Model calculations of q_w as a function of time -- |
| Miscellaneous information |
5.6.5. |
| Title |
Model calculations for total heat load at the stagnation point -- |
| Miscellaneous information |
5.7. |
| Title |
Appendix: Bot Emodeling of non-Orbiter entry problems -- |
| Miscellaneous information |
5.8. |
| Title |
References -- |
| Miscellaneous information |
6. |
| Title |
Estimating the dimensions and performance of the Hubble Space Telescope -- |
| Miscellaneous information |
6.1. |
| Title |
The Hubble Space Telescope -- |
| Miscellaneous information |
6.1.1. |
| Title |
HST system requirements -- |
| Miscellaneous information |
6.1.2. |
| Title |
HST engineering systems -- |
| Miscellaneous information |
6.1.3. |
| Title |
Requirements for fitting the HST into the Orbiter -- |
| Miscellaneous information |
6.2. |
| Title |
The HST Optical Telescope design -- |
| Miscellaneous information |
6.2.1. |
| Title |
The equivalent system focal length -- |
| Miscellaneous information |
6.2.2. |
| Title |
How do designers determine the required system focal ratio, Feq? -- |
| Miscellaneous information |
6.2.3. |
| Title |
Telescope plate scale -- |
| Miscellaneous information |
6.2.4. |
| Title |
Selection of HST's primary mirror focal ratio, F 1 1/4 jf1j=D -- |
| Miscellaneous information |
6.2.5. |
| Title |
Calculating the magnification m and exact constructional length L -- |
| Miscellaneous information |
6.2.6. |
| Title |
Estimating the secondary mirror diameter -- |
| Miscellaneous information |
6.2.7. |
| Title |
Estimating the radius of curvature of the HST secondary mirror -- |
| Miscellaneous information |
6.3. |
| Title |
Modeling the HST length -- |
| Miscellaneous information |
6.3.1. |
| Title |
The light-shield baffle extension -- |
| Miscellaneous information |
6.3.2. |
| Title |
Modeling the length of the light shield -- |
| Miscellaneous information |
6.3.3. |
| Title |
The length of the instrument section -- |
| Miscellaneous information |
6.3.4. |
| Title |
Calculating the total HST telescope length -- |
| Miscellaneous information |
6.4. |
| Title |
Summary of calculated HST dimensions -- |
| Miscellaneous information |
6.5. |
| Title |
Estimating HST mass -- |
| Miscellaneous information |
6.5.1. |
| Title |
Primary mirror design -- |
| Miscellaneous information |
6.5.2. |
| Title |
Estimating primary mirror mass -- |
| Miscellaneous information |
6.5.3. |
| Title |
The estimated total HST system mass and areal density -- |
| Miscellaneous information |
6.5.4. |
| Title |
Some final words on the HST mass estimation exercise -- |
| Miscellaneous information |
6.5.5. |
| Title |
Onward to an estimate of HST's sensitivity -- |
| Miscellaneous information |
6.6. |
| Title |
Back-of-the-Envelope modeling of the HST's sensitivity or signal to noise ratio -- |
| Miscellaneous information |
6.6.1. |
| Title |
Defining signal to noise ratio -- |
| Miscellaneous information |
6.6.2. |
| Title |
Modeling the mean signal, S -- |
| Miscellaneous information |
6.6.3. |
| Title |
Modeling the noise -- |
| Miscellaneous information |
6.6.4. |
| Title |
Final equation for signal to noise ratio -- |
| Miscellaneous information |
6.6.5. |
| Title |
Final thoughts on Bot Eestimates for HST sensitivity -- |
| Miscellaneous information |
6.7. |
| Title |
References. |
| 588 ## - SOURCE OF DESCRIPTION NOTE |
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| Source of description note |
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Aerospace engineering |
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Engineering design. |
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Springer-Praxis books in astronautical engineering. |
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1082775 |
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06-09-21 |
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28-10-15 |
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Book |
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06-04-16 |
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m |
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a |
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eng |
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gw |
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