The Unmanned Space Vehicle test flights use an aircraft with a weight of 1300kg and a length of 7m. The first launch had been planned at the Stratospheric Balloon Launch Facilities of the Italian Space Agency in Trapani-Milo, Sicily. An heavy stratospheric balloon had been chosen to drop the aircraft at the predefined altitude. The aircraft demonstrator after a free fall acceleration to transonic velocity, through a horizontal flight reduces its speed in order to deploy a parachute for an appropriate splash-down into the predefined safe area of the central Mediterranean Sea. The document analyses the failures that could happen during the mission (from pre-flight to the recovery phases), how to recognize them by flight instrumentation and how to mitigate their effects.
Procedure di navigazione missione DTFT0
Cardillo A;Musso I
2006
Abstract
The Unmanned Space Vehicle test flights use an aircraft with a weight of 1300kg and a length of 7m. The first launch had been planned at the Stratospheric Balloon Launch Facilities of the Italian Space Agency in Trapani-Milo, Sicily. An heavy stratospheric balloon had been chosen to drop the aircraft at the predefined altitude. The aircraft demonstrator after a free fall acceleration to transonic velocity, through a horizontal flight reduces its speed in order to deploy a parachute for an appropriate splash-down into the predefined safe area of the central Mediterranean Sea. The document analyses the failures that could happen during the mission (from pre-flight to the recovery phases), how to recognize them by flight instrumentation and how to mitigate their effects.File | Dimensione | Formato | |
---|---|---|---|
prod_160341-doc_130488.pdf
solo utenti autorizzati
Descrizione: Procedure di navigazione missione DTFT0
Dimensione
6.11 kB
Formato
Adobe PDF
|
6.11 kB | Adobe PDF | Visualizza/Apri Richiedi una copia |
I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.