DE68904184T2 - Startverfahren fuer eine sekundaere nutzlast. - Google Patents

Startverfahren fuer eine sekundaere nutzlast.

Info

Publication number
DE68904184T2
DE68904184T2 DE8989200281T DE68904184T DE68904184T2 DE 68904184 T2 DE68904184 T2 DE 68904184T2 DE 8989200281 T DE8989200281 T DE 8989200281T DE 68904184 T DE68904184 T DE 68904184T DE 68904184 T2 DE68904184 T2 DE 68904184T2
Authority
DE
Germany
Prior art keywords
payload
startup procedure
startup
procedure
Prior art date
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.)
Expired - Fee Related
Application number
DE8989200281T
Other languages
English (en)
Other versions
DE68904184D1 (de
Inventor
Kees Jan Sudmeijer
Jan Willem Wegereef
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.)
Fokker Space and Systems BV
Original Assignee
Fokker Space and Systems BV
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 Fokker Space and Systems BV filed Critical Fokker Space and Systems BV
Application granted granted Critical
Publication of DE68904184D1 publication Critical patent/DE68904184D1/de
Publication of DE68904184T2 publication Critical patent/DE68904184T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

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
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1085—Swarms and constellations
    • 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
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641—Interstage or payload connectors

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Automatic Assembly (AREA)
DE8989200281T 1989-02-07 1989-02-07 Startverfahren fuer eine sekundaere nutzlast. Expired - Fee Related DE68904184T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP89200281A EP0381869B1 (de) 1989-02-07 1989-02-07 Startverfahren für eine sekundäre Nutzlast

Publications (2)

Publication Number Publication Date
DE68904184D1 DE68904184D1 (de) 1993-02-11
DE68904184T2 true DE68904184T2 (de) 1993-07-01

Family

ID=8202313

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8989200281T Expired - Fee Related DE68904184T2 (de) 1989-02-07 1989-02-07 Startverfahren fuer eine sekundaere nutzlast.

Country Status (3)

Country Link
EP (1) EP0381869B1 (de)
DE (1) DE68904184T2 (de)
ES (1) ES2038396T3 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2649667B1 (fr) * 1989-07-17 1991-09-20 Centre Nat Etd Spatiales Procede de lancement dans l'espace d'une capsule et moyen de lancement correspondant
FR2735099B1 (fr) * 1995-06-06 1997-08-29 Aerospatiale Dispositif adaptateur basculant pour l'emport de plusieurs charges utiles sur un meme lanceur.
US7036773B2 (en) 2003-08-28 2006-05-02 Ecliptic Enterprises Corporation Compact external launcher for small space payloads
US9758262B2 (en) * 2011-07-20 2017-09-12 The Boeing Company Vented launch vehicle adaptor for a manned spacecraft with “pusher” launch abort system
JP6473004B2 (ja) * 2015-01-21 2019-02-20 株式会社Ｉｈｉエアロスペース 破壊状態観測装置と方法

Also Published As

Publication number Publication date
DE68904184D1 (de) 1993-02-11
ES2038396T3 (es) 1993-07-16
EP0381869B1 (de) 1992-12-30
EP0381869A1 (de) 1990-08-16

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee