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FLPP3-DOC Demise Observation Capsule

Obiettivo

The aim is to build a capsule capable of staying attached to the upper stage of the launch vehicle during its demise in the Earth atmosphere.

Once the needed data have been collected the capsule will separate and will complete an autonomous reentry. After the hypersonic part of the flight, the capsule will transmit the data through the global satellite network IRIDIUM.

Attività nel progetto CIRA

CIRA is in charge of:

  • Definition of the aero-shape.
  • Supervision and consolidation of the aero-thermal database..
  • Design of:
    • Thermal protection systems.
    • Structures.
    • Mechanisms.

More over CIRA, for the parts of responsibility, shall realize:

  • An Engineering Qualification Model, For test and design validation.
  • A Proto-Flight Model for the flight mission

Programma

  • data inizio: Tuesday, December 2, 2014
  • durata: 24.00
Tuesday, September 20, 2016
118
Wednesday, November 23, 2016
FLPP3-DOC
Space - Technology Integration and Flight Demostrators, Aerothermodynamics, Structures and Materials
DOC is an European Project aimed to the design and integration of a first black box prototype for the acquisition of data on the demise of the upper stages of space launch vehicles.
Space Debris
Advanced Materials and Processes

 

 

FLPP3-DOC Demise Observation Capsule<img />https://www.cira.it/en/space/sistemi-di-bordo-per-le-piattaforme-spaziali/flpp3-doc/FLPP3-DOC Demise Observation CapsuleFLPP3-DOC Demise Observation Capsule<p>The aim is to build a capsule capable of staying attached to the upper stage of the launch vehicle during its demise in the Earth atmosphere.</p><p>Once the needed data have been collected the capsule will separate and will complete an autonomous reentry. After the hypersonic part of the flight, the capsule will transmit the data through the global satellite network IRIDIUM.</p><p>CIRA is in charge of:</p><ul><li>Definition of the aero-shape.</li><li>Supervision and consolidation of the aero-thermal database..</li><li>Design of:</li><ul><li>Thermal protection systems.</li><li>Structures.</li><li>Mechanisms.</li></ul></ul><p>More over CIRA, for the parts of responsibility, shall realize:</p><ul><li>An Engineering Qualification Model, For test and design validation.</li><li>A Proto-Flight Model for the flight mission</li></ul>2014-12-01T23:00:00Z24.0000000000000

 Media gallery

 

 

Parte della capsula DOC realizzata in lega di titanio per prototipazione rapida.https://www.cira.it/PublishingImages/Forms/DispForm.aspx?ID=831Parte della capsula DOC realizzata in lega di titanio per prototipazione rapida.Imagehttps://www.cira.it/PublishingImages/DOC%20ALM%20Part%202.png
DOC CATIA Modelhttps://www.cira.it/PublishingImages/Forms/DispForm.aspx?ID=240DOC CATIA ModelImagehttps://www.cira.it/PublishingImages/DOC%20CATIA%20Model.png
Profilo di missione della capsula DOChttps://www.cira.it/PublishingImages/Forms/DispForm.aspx?ID=830Profilo di missione della capsula DOCImagehttps://www.cira.it/PublishingImages/DOC%20Profilo%20Missione.png

 Activities