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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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Kaydedildi:
Detaylı Bibliyografya
Asıl Yazarlar: Karp, Ashley Chandler (Yazar), Jens, Elizabeth Therese (Yazar)
Materyal Türü: Elektronik Ekitap
Dil:İngilizce
Baskı/Yayın Bilgisi: Amsterdam : Academic Press, 2023.
Konular:
Hybrid propellant rockets > Design and construction.
Online Erişim:ScienceDirect
Etiketler: Etiketle
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İçindekiler:
  • 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
  • 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
  • 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
  • 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
  • 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

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