ITUB20160826A1 - BRAKE SATELLITE AND THERMAL PROTECTION THAT CAN BE CONTROLLED IN A CONTROLLED WAY - Google Patents

BRAKE SATELLITE AND THERMAL PROTECTION THAT CAN BE CONTROLLED IN A CONTROLLED WAY

Info

Publication number
ITUB20160826A1
ITUB20160826A1 ITUB2016A000826A ITUB20160826A ITUB20160826A1 IT UB20160826 A1 ITUB20160826 A1 IT UB20160826A1 IT UB2016A000826 A ITUB2016A000826 A IT UB2016A000826A IT UB20160826 A ITUB20160826 A IT UB20160826A IT UB20160826 A1 ITUB20160826 A1 IT UB20160826A1
Authority
IT
Italy
Prior art keywords
controlled
satellite
brake
thermal protection
way
Prior art date
Application number
ITUB2016A000826A
Other languages
Italian (it)
Inventor
Stefano Pagano
Original Assignee
Stefano Pagano
Savino Raffaele
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Stefano Pagano, Savino Raffaele filed Critical Stefano Pagano
Priority to ITUB2016A000826A priority Critical patent/ITUB20160826A1/en
Publication of ITUB20160826A1 publication Critical patent/ITUB20160826A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/52Protection, safety or emergency devices; Survival aids
    • B64G1/58Thermal protection, e.g. heat shields
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/62Systems for re-entry into the earth's atmosphere; Retarding or landing devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Critical Care (AREA)
  • Emergency Medicine (AREA)
  • General Health & Medical Sciences (AREA)
ITUB2016A000826A 2016-02-18 2016-02-18 BRAKE SATELLITE AND THERMAL PROTECTION THAT CAN BE CONTROLLED IN A CONTROLLED WAY ITUB20160826A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ITUB2016A000826A ITUB20160826A1 (en) 2016-02-18 2016-02-18 BRAKE SATELLITE AND THERMAL PROTECTION THAT CAN BE CONTROLLED IN A CONTROLLED WAY

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITUB2016A000826A ITUB20160826A1 (en) 2016-02-18 2016-02-18 BRAKE SATELLITE AND THERMAL PROTECTION THAT CAN BE CONTROLLED IN A CONTROLLED WAY

Publications (1)

Publication Number Publication Date
ITUB20160826A1 true ITUB20160826A1 (en) 2016-05-18

Family

ID=56618211

Family Applications (1)

Application Number Title Priority Date Filing Date
ITUB2016A000826A ITUB20160826A1 (en) 2016-02-18 2016-02-18 BRAKE SATELLITE AND THERMAL PROTECTION THAT CAN BE CONTROLLED IN A CONTROLLED WAY

Country Status (1)

Country Link
IT (1) ITUB20160826A1 (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1905691A1 (en) * 2006-09-30 2008-04-02 Astrium GmbH Deployable braking structure for space vehicles
US8292232B1 (en) * 2009-08-11 2012-10-23 Andrews Space, Inc. Deployable decelerator based microsatellite recovery
US8733706B1 (en) * 2012-05-15 2014-05-27 The United States of America as represented by the Administrator of the National Aeronautics & Space Administration (NASA) Transformable and reconfigurable entry, descent and landing systems and methods

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1905691A1 (en) * 2006-09-30 2008-04-02 Astrium GmbH Deployable braking structure for space vehicles
US8292232B1 (en) * 2009-08-11 2012-10-23 Andrews Space, Inc. Deployable decelerator based microsatellite recovery
US8733706B1 (en) * 2012-05-15 2014-05-27 The United States of America as represented by the Administrator of the National Aeronautics & Space Administration (NASA) Transformable and reconfigurable entry, descent and landing systems and methods

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
MAGAZU H K ET AL: "AEROTHERMODYNAMICS OF A PARASHIELD RE-ENTRY VEHICLE", JOURNAL OF SPACECRAFT AND ROCKETS, AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS,REASTON,VA, US, vol. 35, no. 4, 1 July 1998 (1998-07-01), pages 434 - 441, XP000772988, ISSN: 0022-4650 *
MARRAFFA L ET AL: "INFLATABLE RE-ENTRY TECHNOLOGIES: FLIGHT DEMONSTRATION AND FUTURE PROSPECTS", ESA BULLETIN, ESA SCIENTIFIC AND PUBLICATIONS BRANCH, NOORDWIJK, NL, no. 103, 1 August 2000 (2000-08-01), pages 78 - 85, XP000966642, ISSN: 0376-4265 *
MATTHIAS WIEGAND ET AL: "A Small Re-entry Capsule -BREM-SAT 2", PROCEEDINGS OF THE 10TH AIAA/USU SMALL SATELLITE CONFERENCE, LOGAN, 1 January 1996 (1996-01-01), XP055224098, Retrieved from the Internet <URL:http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=2469&context=smallsat> [retrieved on 20151028] *

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