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Cycle 0(CY1991) NLS trade studies and analyses report
| Cycle 0(CY1991) NLS trade studies and analyses report |
| Pubbl/distr/stampa | [New Orleans, LA] : , : National Aeronautics and Space Administration, Marshall Space Flight Center, Michoud Assembly Facility, , January 1992 |
| Descrizione fisica | 1 online resource (2 volumes) : illustrations |
| Collana | NASA-CR |
| Soggetto topico |
Cryogenic fluid storage
Fuel tank pressurization Liquid hydrogen Liquid oxygen Liquid propellant rocket engines Space transportation system |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | bk. I. Structures & core vehicle. -- bk. II, pt. 2. Propuslion. |
| Altri titoli varianti | Cycle 0 |
| Record Nr. | UNINA-9910703613403321 |
| [New Orleans, LA] : , : National Aeronautics and Space Administration, Marshall Space Flight Center, Michoud Assembly Facility, , January 1992 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Formed platelet liner construction feasibility / prepared by: W.A. Hays, D.E. Janke
| Formed platelet liner construction feasibility / prepared by: W.A. Hays, D.E. Janke |
| Autore | Hays W. A. |
| Pubbl/distr/stampa | Marshall Space Flight Center, AL : , : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, , September 1992 |
| Descrizione fisica | 1 online resource (vii, 140 pages, 20 unnumbered pages) : illustrations |
| Collana | NASA-CR |
| Soggetto topico |
Combustion chambers
Liquid propellant rocket engines Regenerative cooling Rocket linings Feasibility analysis |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Formed platelet liner construction feasibility / prepared by |
| Record Nr. | UNINA-9910703614203321 |
Hays W. A.
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| Marshall Space Flight Center, AL : , : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, , September 1992 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Fundamental concepts of liquid-propellant rocket engines / / Alessandro de Iaco Veris
| Fundamental concepts of liquid-propellant rocket engines / / Alessandro de Iaco Veris |
| Autore | De Iaco Veris Alessandro |
| Edizione | [1st ed. 2021.] |
| Pubbl/distr/stampa | Cham, Switzerland : , : Springer, , [2021] |
| Descrizione fisica | 1 online resource (IX, 747 p. 456 illus., 57 illus. in color.) |
| Disciplina | 621.4356 |
| Collana | Springer Aerospace Technology |
| Soggetto topico | Liquid propellant rocket engines |
| ISBN | 3-030-54704-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Preface -- Chapter 1: Fundamental concepts on liquid-propellant rocket Engines -- Chapter 2: The thrust chamber assembly -- Chapter 3: Feed systems using gases under pressure -- Chapter 4: Feed systems using turbo-pumps -- Chapter 5: Control systems and valves -- Chapter 6: Tanks for propellants -- Chapter 7: Interconnecting components and structures. |
| Record Nr. | UNINA-9910484007503321 |
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De Iaco Veris Alessandro
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| Cham, Switzerland : , : Springer, , [2021] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Internal combustion processes of liquid rocket engines : modeling and numerical simulations / / Zhen-Guo Wang
| Internal combustion processes of liquid rocket engines : modeling and numerical simulations / / Zhen-Guo Wang |
| Autore | Wang Zhen-Guo |
| Pubbl/distr/stampa | Singapore : , : Wiley, , 2016 |
| Descrizione fisica | 1 online resource (395 p.) |
| Disciplina | 629.47522 |
| Soggetto topico |
Liquid propellant rockets
Liquid propellant rocket engines |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-118-89005-1
1-118-89004-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Title Page ; Copyright Page ; Contents; Preface; Chapter 1 Introduction ; 1.1 Basic Configuration of Liquid Rocket Engines; 1.1.1 Propellant Feed System; 1.1.2 Thrust Chamber; 1.2 Internal Combustion Processes of Liquid Rocket Engines; 1.2.1 Start and Shutdown; 1.2.2 Combustion Process; 1.2.3 Performance Parameters in Working Process; 1.3 Characteristics and Development History of Numerical Simulation of the Combustion Process in Liquid Rocket Engines; 1.3.1 Benefits of Numerical Simulation of the Combustion Process in Liquid Rocket Engines
1.3.2 Main Contents of Numerical Simulations of Liquid Rocket Engine Operating Process1.3.3 Development of Numerical Simulations of Combustion Process in Liquid Rocket Engines; 1.4 Governing Equations of Chemical Fluid Dynamics; 1.5 Outline of this Book; References; Chapter 2 Physical Mechanism and Numerical Modeling of Liquid Propellant Atomization ; 2.1 Types and Functions of Injectors in a Liquid Rocket Engine; 2.2 Atomization Mechanism of Liquid Propellant; 2.2.1 Formation of Static Liquid Droplet; 2.2.2 Breakup of Cylindrical Liquid Jet; 2.2.3 Liquid Sheet Breakup 2.2.4 Droplet Secondary Breakup2.3 Characteristics of Atomization in Liquid Rocket Engines; 2.3.1 Distribution Function of the Droplet Size; 2.3.2 Mean Diameter and Characteristic Diameter; 2.3.3 Measurement of Spray Size Distribution; 2.4 Atomization Modeling for Liquid Rocket Engine Atomizers; 2.4.1 Straight-flow Injector; 2.4.2 Centrifugal Injector; 2.4.3 Impinging-stream Injectors; 2.4.4 Coaxial Shear Injector; 2.4.5 Coaxial Centrifugal Injectors; 2.5 Numerical Simulation of Liquid Propellant Atomization; 2.5.1 Theoretical Models of Liquid Propellant Atomization; 2.5.2 Quasi-fluid Models 2.5.3 Particle Trajectory Models2.5.4 Simulation of Liquid Jet Atomization Using Interface Tracking Method; 2.5.5 Liquid Jet Structure - Varying Flow Conditions; References; Chapter 3 Modeling of Droplet Evaporation and Combustion ; 3.1 Theory for Quasi-Steady Evaporation and Combustion of a Single Droplet at Atmospheric Pressure; 3.1.1 Quasi-Steady Evaporation Theory for Single Droplet in the Static Gas without Combustion; 3.1.2 Quasi-Steady Evaporation Theory for Droplet in a Static Gas with Combustion; 3.1.3 Non-Combustion Evaporation Theory for a Droplet in a Convective Flow 3.1.4 Evaporation Theory for a Droplet in a Convective Medium with Combustion3.2 Evaporation Model for a Single Droplet under High Pressure; 3.2.1 ZKS Droplet High Pressure Evaporation Theory; 3.2.2 Application of the Liquid Activity Coefficient to Calculate the Gas-Liquid Equilibrium at a High Pressure; 3.3 Subcritical Evaporation Response Characteristics of Propellant Droplet in Oscillatory Environments; 3.3.1 Physical Model; 3.3.2 Examples and the Analysis of Results; 3.4 Multicomponent Fuel Droplet Evaporation Model; 3.4.1 Simple Multicomponent Droplet Evaporation Model 3.4.2 Continuous Thermodynamics Model of Complex Multicomponent Mixture Droplet Evaporation |
| Record Nr. | UNINA-9910136758203321 |
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Wang Zhen-Guo
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| Singapore : , : Wiley, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Internal combustion processes of liquid rocket engines : modeling and numerical simulations / / Zhen-Guo Wang
| Internal combustion processes of liquid rocket engines : modeling and numerical simulations / / Zhen-Guo Wang |
| Autore | Wang Zhen-Guo |
| Pubbl/distr/stampa | Singapore : , : Wiley, , 2016 |
| Descrizione fisica | 1 online resource (395 p.) |
| Disciplina | 629.47522 |
| Soggetto topico |
Liquid propellant rockets
Liquid propellant rocket engines |
| ISBN |
1-118-89005-1
1-118-89004-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Title Page ; Copyright Page ; Contents; Preface; Chapter 1 Introduction ; 1.1 Basic Configuration of Liquid Rocket Engines; 1.1.1 Propellant Feed System; 1.1.2 Thrust Chamber; 1.2 Internal Combustion Processes of Liquid Rocket Engines; 1.2.1 Start and Shutdown; 1.2.2 Combustion Process; 1.2.3 Performance Parameters in Working Process; 1.3 Characteristics and Development History of Numerical Simulation of the Combustion Process in Liquid Rocket Engines; 1.3.1 Benefits of Numerical Simulation of the Combustion Process in Liquid Rocket Engines
1.3.2 Main Contents of Numerical Simulations of Liquid Rocket Engine Operating Process1.3.3 Development of Numerical Simulations of Combustion Process in Liquid Rocket Engines; 1.4 Governing Equations of Chemical Fluid Dynamics; 1.5 Outline of this Book; References; Chapter 2 Physical Mechanism and Numerical Modeling of Liquid Propellant Atomization ; 2.1 Types and Functions of Injectors in a Liquid Rocket Engine; 2.2 Atomization Mechanism of Liquid Propellant; 2.2.1 Formation of Static Liquid Droplet; 2.2.2 Breakup of Cylindrical Liquid Jet; 2.2.3 Liquid Sheet Breakup 2.2.4 Droplet Secondary Breakup2.3 Characteristics of Atomization in Liquid Rocket Engines; 2.3.1 Distribution Function of the Droplet Size; 2.3.2 Mean Diameter and Characteristic Diameter; 2.3.3 Measurement of Spray Size Distribution; 2.4 Atomization Modeling for Liquid Rocket Engine Atomizers; 2.4.1 Straight-flow Injector; 2.4.2 Centrifugal Injector; 2.4.3 Impinging-stream Injectors; 2.4.4 Coaxial Shear Injector; 2.4.5 Coaxial Centrifugal Injectors; 2.5 Numerical Simulation of Liquid Propellant Atomization; 2.5.1 Theoretical Models of Liquid Propellant Atomization; 2.5.2 Quasi-fluid Models 2.5.3 Particle Trajectory Models2.5.4 Simulation of Liquid Jet Atomization Using Interface Tracking Method; 2.5.5 Liquid Jet Structure - Varying Flow Conditions; References; Chapter 3 Modeling of Droplet Evaporation and Combustion ; 3.1 Theory for Quasi-Steady Evaporation and Combustion of a Single Droplet at Atmospheric Pressure; 3.1.1 Quasi-Steady Evaporation Theory for Single Droplet in the Static Gas without Combustion; 3.1.2 Quasi-Steady Evaporation Theory for Droplet in a Static Gas with Combustion; 3.1.3 Non-Combustion Evaporation Theory for a Droplet in a Convective Flow 3.1.4 Evaporation Theory for a Droplet in a Convective Medium with Combustion3.2 Evaporation Model for a Single Droplet under High Pressure; 3.2.1 ZKS Droplet High Pressure Evaporation Theory; 3.2.2 Application of the Liquid Activity Coefficient to Calculate the Gas-Liquid Equilibrium at a High Pressure; 3.3 Subcritical Evaporation Response Characteristics of Propellant Droplet in Oscillatory Environments; 3.3.1 Physical Model; 3.3.2 Examples and the Analysis of Results; 3.4 Multicomponent Fuel Droplet Evaporation Model; 3.4.1 Simple Multicomponent Droplet Evaporation Model 3.4.2 Continuous Thermodynamics Model of Complex Multicomponent Mixture Droplet Evaporation |
| Record Nr. | UNINA-9910830290403321 |
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Wang Zhen-Guo
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| Singapore : , : Wiley, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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NASA's chemical transfer propulsion program for Pathfinder [[electronic resource] /] / Ned P. Hannum and Frank D. Berkopec, and Robert L. Zurawski
| NASA's chemical transfer propulsion program for Pathfinder [[electronic resource] /] / Ned P. Hannum and Frank D. Berkopec, and Robert L. Zurawski |
| Autore | Hannum Ned P |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, , [1989] |
| Descrizione fisica | 16 pages : digital, PDF file |
| Altri autori (Persone) |
BerkopecFrank D
ZurawskiR. L |
| Collana | NASA technical memorandum |
| Soggetto topico |
Chemical propulsion
Landing modules Liquid propellant rocket engines Manned spacecraft NASA programs Orbit transfer vehicles Project management Rocket engine design Space exploration Space programs Spacecraft propulsion |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697914503321 |
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Hannum Ned P
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, , [1989] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A review of the supply of liquid propellants and other fluids in support of the space shuttle program [[electronic resource] /] / Stacy E. Churchwell
| A review of the supply of liquid propellants and other fluids in support of the space shuttle program [[electronic resource] /] / Stacy E. Churchwell |
| Autore | Churchwell Stacy E |
| Pubbl/distr/stampa | [Kennedy Space Center, Fla.] : , : National Aeronautics and Space Administration, John F. Kennedy Space Center, , [1989] |
| Descrizione fisica | vii, 41 pages : digital, PDF file |
| Collana | NASA technical memorandum |
| Soggetto topico |
Liquid propellant rocket engines
Liquid rocket propellants Logistics management Propellant storage Space Shuttle Main Engine |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697903703321 |
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Churchwell Stacy E
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| [Kennedy Space Center, Fla.] : , : National Aeronautics and Space Administration, John F. Kennedy Space Center, , [1989] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Study of basic physical processes in liquid rocket engines / / by S.T. Wu and C.P. Chen
| Study of basic physical processes in liquid rocket engines / / by S.T. Wu and C.P. Chen |
| Autore | Wu S. T (Shi-Tsan), <1933-> |
| Pubbl/distr/stampa | Huntsville, AL : , : NASA/Marshall Space Flight Center, , September 1992 |
| Descrizione fisica | 1 online resource (i, 48 pages) |
| Collana | NASA-CR |
| Soggetto topico |
Computational fluid dynamics
Liquid propellant rocket engines Navier-Stokes equation Propellant combustion Reacting flow Thermodynamic equilibrium |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702893303321 |
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Wu S. T (Shi-Tsan), <1933->
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| Huntsville, AL : , : NASA/Marshall Space Flight Center, , September 1992 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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