AU2001252887A1 - Aerodynamic fairing - Google Patents

Aerodynamic fairing

Info

Publication number: AU2001252887A1
Authority: AU; Australia
Prior art keywords: aerodynamic fairing; fairing; aerodynamic
Prior art date: 2000-02-29
Legal status (The legal status 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 status listed.): Abandoned

Application number

AU2001252887A

Inventor

Michael J. Schoonmaker

George Sowers

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Lockheed Martin Corp

Original Assignee

Lockheed Corp

Lockheed Martin Corp

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.)

2000-02-29

Filing date

2001-02-28

Publication date

2001-09-12

2001-02-28 Application filed by Lockheed Corp, Lockheed Martin Corp filed Critical Lockheed Corp

2001-09-12 Publication of AU2001252887A1 publication Critical patent/AU2001252887A1/en

Status Abandoned legal-status Critical Current

Classifications

- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/228—Damping of high-frequency vibration effects on spacecraft elements, e.g. by using acoustic vibration dampers

Landscapes

Engineering & Computer Science (AREA)
Remote Sensing (AREA)
Aviation & Aerospace Engineering (AREA)
Physics & Mathematics (AREA)
Acoustics & Sound (AREA)
Laminated Bodies (AREA)
Structures Of Non-Positive Displacement Pumps (AREA)

AU2001252887A 2000-02-29 2001-02-28 Aerodynamic fairing Abandoned AU2001252887A1 (en)

Applications Claiming Priority (3)

Application Number	Priority Date	Filing Date	Title
US18591500P	2000-02-29	2000-02-29
US60185915		2000-02-29
PCT/US2001/006336 WO2001064509A2 (en)	2000-02-29	2001-02-28	Aerodynamic fairing

Publications (1)

Publication Number	Publication Date
AU2001252887A1 true AU2001252887A1 (en)	2001-09-12

Family

ID=22682942

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
AU2001252887A Abandoned AU2001252887A1 (en)	2000-02-29	2001-02-28	Aerodynamic fairing

Country Status (5)

Country	Link
US (1)	US6554228B2 (en)
EP (1)	EP1259425A2 (en)
JP (1)	JP2003525171A (en)
AU (1)	AU2001252887A1 (en)
WO (1)	WO2001064509A2 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US6557803B2 (en) *	2001-08-31	2003-05-06	The Boeing Company	Crewed on-orbit, returnable, and reusable space vehicle
US20030052232A1 (en) *	2001-09-17	2003-03-20	Hall Allison Earl	Space transportation system
US6802179B2 (en)	2002-12-02	2004-10-12	Aerojet-General Corporation	Nozzle with spiral internal cooling channels
US6799417B2 (en)	2003-02-05	2004-10-05	Aerojet-General Corporation	Diversion of combustion gas within a rocket engine to preheat fuel
US20070163228A1 (en) *	2006-01-19	2007-07-19	United Technologies Corporation	Gas augmented rocket engine
CN103455646A (en) *	2012-05-31	2013-12-18	北京宇航系统工程研究所	Main binding connection structure dynamic simulation method
FR2998269B1 (en) *	2012-11-20	2015-01-02	Centre Nat Detudes Spatiales Cnes	CONNECTING DEVICE BETWEEN A FIRST FLOOR AND A SECOND FLOOR OF A COMPOSITE BELOW A LAUNCHER; LAUNCHER, LAUNCHING METHOD, AND ASSOCIATED ASSEMBLY METHODS
US20150048212A1 (en) *	2013-08-19	2015-02-19	The Boeing Company	Unsteady aerodynamics mitigation for multi-body aerospace apparatus
CN106055748B (en) *	2016-05-23	2019-02-05	北京理工大学	A Parametric Determination Method for the Binding Position of Solid Binding Rockets

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US4650139A (en)	1984-07-31	1987-03-17	Taylor Thomas C	Aerospike for attachment to space vehicle system
US4884770A (en)	1987-07-23	1989-12-05	The United States Of America As Represented By The National Aeronautics And Space Administration	Earth-to-orbit vehicle providing a reusable orbital stage
US4850275A (en)	1987-10-30	1989-07-25	The Bdm Corporation	Aircraft hollow nose cone
US5242135A (en) *	1990-01-30	1993-09-07	Scott David R	Space transfer vehicle and integrated guidance launch system
FR2664563B1 (en)	1990-07-11	1992-10-30	Aerospatiale	FRONT END STRUCTURE OF A BOOSTER PROPELLER MOUNTED ON THE MAIN BODY OF A LAUNCHER.
US5143327A (en) *	1990-08-31	1992-09-01	The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration	Integrated launch and emergency vehicle system

2001
- 2001-02-28 AU AU2001252887A patent/AU2001252887A1/en not_active Abandoned
- 2001-02-28 EP EP01926344A patent/EP1259425A2/en not_active Withdrawn
- 2001-02-28 JP JP2001563376A patent/JP2003525171A/en active Pending
- 2001-02-28 WO PCT/US2001/006336 patent/WO2001064509A2/en not_active Ceased
- 2001-02-28 US US09/795,221 patent/US6554228B2/en not_active Expired - Fee Related

Also Published As

Publication number	Publication date
EP1259425A2 (en)	2002-11-27
JP2003525171A (en)	2003-08-26
WO2001064509A2 (en)	2001-09-07
US20020104928A1 (en)	2002-08-08
WO2001064509A3 (en)	2002-01-03
US6554228B2 (en)	2003-04-29

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