1.

Record Nr.

UNISA996216748803316

Titolo

2011 3rd International Congress on Engineering Education

Pubbl/distr/stampa

[Place of publication not identified], : IEEE, 2012

ISBN

1-4577-1259-8

Descrizione fisica

1 online resource (222 pages)

Disciplina

620.00711

Soggetti

Engineering - Study and teaching

Lingua di pubblicazione

Inglese

Formato

Materiale a stampa

Livello bibliografico

Monografia

Note generali

Bibliographic Level Mode of Issuance: Monograph

2.

Record Nr.

UNINA9910967539703321

Autore

Micci Michael M (Michael Matthew)

Titolo

Micropropulsion for small spacecraft / / edited by Michael M. Micci, Andrew D. Ketsdever

Pubbl/distr/stampa

Reston, Va., : American Institute of Aeronautics and Astronautics, c2000

ISBN

1-60086-658-1

1-60086-439-2

Edizione

[1st ed.]

Descrizione fisica

1 online resource (496 p.)

Collana

Progress in astronautics and aeronautics ; ; v. 187

Altri autori (Persone)

MicciMichael M (Michael Matthew)

KetsdeverAndrew D (Andrew David)

Disciplina

629.47/5

Soggetti

Microspacecraft

Space vehicles - Propulsion systems

Rocket engines - Thrust

Lingua di pubblicazione

Inglese

Formato

Materiale a stampa

Livello bibliografico

Monografia

Note generali

Description based upon print version of record.

Nota di bibliografia

Includes bibliographical references and author index.



Nota di contenuto

Surveys -- Electrothermal thrusters -- Electrostatic thrusters -- Electromagnetic thrusters -- Components.

Sommario/riassunto

Micropropulsion is an enabling technology for microspacecraft operations by making missions possible which otherwise could not be performed. For example, the formation and maintenance of platoons of microspacecraft will require a manoeuvering capability to counter orbital perturbations. Microspacecraft missions involving large spacecraft resupply, repair or surveillance will also require manoeuverability. The mission requirements for microspacecraft will be varied and in some cases a large range of capability might be required on the same spacecraft. Micropropulsion systems must be extremely versatile to address these requirements.