Hybrid rocket propulsion design handbook
Hybrid Rocket Propulsion Design Handbook provides system scaling laws, design methodologies, and a summary of available test data, giving engineers all the tools they need to develop realistic hybrid system designs.Important supporting theory from chemistry, thermodynamics, and rocket propulsion is...
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| Autors principals: | , |
|---|---|
| Format: | Electrònic eBook |
| Idioma: | anglès |
| Publicat: |
Amsterdam :
Academic Press,
2023.
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| Matèries: | |
| Accés en línia: | ScienceDirect |
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| 020 | |a 9780128165935 |z 9780128161999 (pbk.) : |q (e-book) | ||
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| 082 | 0 | 4 | |a 629.475 |2 23 |1 https://id.oclc.org/worldcat/ddc/E346Gd9yfG4qr9vk46QPmgXYTV |
| 100 | 1 | |a Karp, Ashley Chandler, |e author. | |
| 245 | 1 | 0 | |a Hybrid rocket propulsion design handbook |c Ashley Chandler Karp, Elizabeth Therese Jens. |
| 264 | 1 | |a Amsterdam : |b Academic Press, |c 2023. | |
| 300 | |a 1 online resource | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 520 | |a Hybrid Rocket Propulsion Design Handbook provides system scaling laws, design methodologies, and a summary of available test data, giving engineers all the tools they need to develop realistic hybrid system designs.Important supporting theory from chemistry, thermodynamics, and rocket propulsion is addressed, helping readers from a variety of backgrounds to understand this interdisciplinary subject. This book also suggests guidelines for standardized reporting of test data, in response to difficulties researchers have in working with results from different research institutes. | ||
| 505 | 0 | |a Front Cover -- Hybrid Rocket Propulsion Design Handbook -- Copyright -- Dedication -- Contents -- List of tables -- List of figures -- Nomenclature -- 1 Introduction -- 1.1 Chemical propulsion overview -- 1.2 What is a hybrid rocket? -- 1.3 Comparison of chemical propulsion systems -- 1.4 Benefits and challenges of hybrid propulsion systems -- 1.4.1 Benefits -- 1.4.2 Challenges and mitigations -- 1.5 Applications -- 1.6 History and current programs -- 1.6.1 Early hybrid rockets, 1930s-1940s -- 1.6.2 Sandpiper, 1960s -- 1.6.3 Teledyne XAQM-81A firebolt supersonic aerial target, 1970s | |
| 505 | 8 | |a 1.6.4 Booster scale hybrid rockets -- AMROC -- HDPD, 1990s -- 1.6.5 HYSR, 2002 -- 1.6.6 SpaceShipOne (2004) and SpaceShipTwo (2010-2021) -- 1.6.7 Falcon -- 1.6.8 Peregrine, 2000s to 2010s -- 1.6.9 Space Propulsion Group -- 1.6.10 Mars Ascent Vehicle, 2010s -- 1.6.11 Nucleus, NAMMO -- 1.6.12 HyImpulse Technologies, Germany -- 1.6.13 Gilmour Space Technologies, Australia -- 1.6.14 Taiwan Innovation Space (TiSPACE), Taiwan -- 1.6.15 Delta V Space Technologies, Turkey -- 1.6.16 SpaceForest, Poland -- 1.6.17 SpaceRyde, Canada -- 1.6.18 University research and sounding rockets | |
| 505 | 8 | |a 1.7 Commonly used terms -- 1.8 Book layout -- 2 Introduction to rocket propulsion -- 2.1 Introduction -- 2.2 Key parameters -- 2.2.1 Thrust -- 2.2.2 Thrust coefficient -- 2.2.3 Propellant mass flow rate -- 2.2.4 Characteristic velocity -- 2.2.5 Effective exhaust velocity -- 2.2.6 Specific impulse -- 2.2.7 Total impulse -- 2.2.8 Density impulse -- 2.2.9 Characteristic chamber length -- 2.2.10 Relationship between key parameters -- 2.3 Nozzles -- 2.4 Rocket equation -- 2.4.1 Launch mission design -- 2.4.2 Gravity losses -- 2.4.3 Aerodynamic forces -- 2.4.4 Oberth effect -- 2.5 Examples of V's | |
| 505 | 8 | |a 2.5.1 Launch to orbit -- 2.5.2 Hohmann transfers to estimate V's -- 2.6 Staging -- 3 Hybrid rocket theory -- 3.1 Introduction -- 3.2 Classical fuels theory -- 3.2.1 Dimensionless parameters -- 3.2.2 Regression rate -- Accounting for radiative heat transfer -- 3.2.3 Estimation of blowing parameter and flame location -- 3.2.4 Classical theory limitations -- 3.3 Liquefying fuels -- 3.3.1 Melt layer thickness -- 3.3.2 Regression rate -- 3.3.3 Properties -- 3.4 Theory applied to single port hybrid design -- 3.4.1 Complete solutions to predict performance -- 3.4.2 Simplified governing equations | |
| 505 | 8 | |a 3.4.3 O/F shift -- 3.5 Regression rate enhancements -- 3.5.1 Swirl injection hybrids -- 3.5.2 Other techniques -- Impinging designs -- Pressure dependent designs -- Aft injection -- Turbulence -- 3.6 Transients -- 3.6.1 Quasi-steady transients -- 3.6.2 Combustion instability transients -- 4 Thermodynamics and chemistry -- 4.1 Introduction -- 4.1.1 Combustion -- 4.1.2 Nozzle -- 4.2 Key terms -- 4.3 Ideal gas mixtures -- 4.4 Real gases -- 4.5 Enthalpy -- 4.5.1 Latent heat of vaporization -- 4.5.2 Enthalpy of formation -- 4.5.3 Bond additivity -- 4.6 Stoichiometry and complete combustion | |
| 650 | 0 | |a Hybrid propellant rockets |x Design and construction. | |
| 700 | 1 | |a Jens, Elizabeth Therese, |e author. | |
| 776 | 0 | 8 | |i Print version: |a Chandler Karp, Ashley |t Hybrid Rocket Propulsion Design Handbook |d San Diego : Elsevier Science & Technology,c2023 |z 9780128161999 |
| 856 | 4 | 0 | |3 ScienceDirect |u https://www.sciencedirect.com/science/book/9780128161999 |