Annular slit colloid thruster research and development / / by Kenneth W. Stark and William A. Burton
| Annular slit colloid thruster research and development / / by Kenneth W. Stark and William A. Burton |
| Autore | Stark Kenneth W. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , May 1971 |
| Descrizione fisica | 1 online resource (v, 56 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Aerospace vehicles
Propellants Rocket engines Rocket engines - Thrust Space vehicles - Propulsion systems |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716001703321 |
Stark Kenneth W.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , May 1971 | ||
| Lo trovi qui: Univ. Federico II | ||
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Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines / / by Reino J. Salmi, John P. Wanhainen, and Ned P. Hannum
| Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines / / by Reino J. Salmi, John P. Wanhainen, and Ned P. Hannum |
| Autore | Salmi Reino J. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 |
| Descrizione fisica | 1 online resource (ii, 27 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Rocket engines - Combustion
Rocket engines - Thrust |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714071603321 |
Salmi Reino J.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 | ||
| Lo trovi qui: Univ. Federico II | ||
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Micropropulsion for small spacecraft [[electronic resource] /] / edited by Michael M. Micci, Andrew D. Ketsdever
| Micropropulsion for small spacecraft [[electronic resource] /] / edited by Michael M. Micci, Andrew D. Ketsdever |
| Autore | Micci Michael M (Michael Matthew) |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2000 |
| Descrizione fisica | 1 online resource (496 p.) |
| Disciplina | 629.47/5 |
| Altri autori (Persone) |
MicciMichael M (Michael Matthew)
KetsdeverAndrew D (Andrew David) |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Microspacecraft
Space vehicles - Propulsion systems Rocket engines - Thrust |
| ISBN |
1-60086-658-1
1-60086-439-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Surveys -- Electrothermal thrusters -- Electrostatic thrusters -- Electromagnetic thrusters -- Components. |
| Record Nr. | UNINA-9910781700503321 |
Micci Michael M (Michael Matthew)
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| Reston, Va., : American Institute of Aeronautics and Astronautics, c2000 | ||
| Lo trovi qui: Univ. Federico II | ||
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Micropropulsion for small spacecraft [[electronic resource] /] / edited by Michael M. Micci, Andrew D. Ketsdever
| Micropropulsion for small spacecraft [[electronic resource] /] / edited by Michael M. Micci, Andrew D. Ketsdever |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2000 |
| Descrizione fisica | 1 online resource (496 p.) |
| Disciplina | 629.47/5 |
| Altri autori (Persone) |
MicciMichael M (Michael Matthew)
KetsdeverAndrew D (Andrew David) |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Microspacecraft
Space vehicles - Propulsion systems Rocket engines - Thrust |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-658-1
1-60086-439-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Surveys -- Electrothermal thrusters -- Electrostatic thrusters -- Electromagnetic thrusters -- Components. |
| Record Nr. | UNINA-9910457230803321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, c2000 | ||
| Lo trovi qui: Univ. Federico II | ||
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