PUMA
Istituto di Scienza e Tecnologie dell'Informazione     
De Micco A., Cardillo A., Musso I. Balloon flight analysis missione USV_DTFT0. Il lavoro del personale CNR-ISTI stato effettuato nell'ambito del contratto ASI N. I/019/05/0. Technical report, 2006.
 
 
Abstract
(English)
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 contains the general flight rules of the USV_DTFT0 mission (Operating Limitation; Equipment Requirements; Termination; Flight Notification; Position Recording and Report Rules).
URL: http://www.asi.it/
Subject Balloon flight rules
Balloon flight notification
Balloon light operating limitation
Balloon flight equipment requirements
Balloon flight position recording
J.2 Physical sciences and engineering. Aerospace


Icona documento 1) Download Document PDF


Icona documento Open access Icona documento Restricted Icona documento Private

 


Per ulteriori informazioni, contattare: Librarian http://puma.isti.cnr.it

Valid HTML 4.0 Transitional