JPS6483500A - Rocket with auxiliary booster separator - Google Patents

Rocket with auxiliary booster separator

Info

Publication number
JPS6483500A
JPS6483500A JP62237092A JP23709287A JPS6483500A JP S6483500 A JPS6483500 A JP S6483500A JP 62237092 A JP62237092 A JP 62237092A JP 23709287 A JP23709287 A JP 23709287A JP S6483500 A JPS6483500 A JP S6483500A
Authority
JP
Japan
Prior art keywords
auxiliary booster
main body
rocket
time
rocket main
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.)
Pending
Application number
JP62237092A
Other languages
Japanese (ja)
Inventor
Hideki Nomoto
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP62237092A priority Critical patent/JPS6483500A/en
Publication of JPS6483500A publication Critical patent/JPS6483500A/en
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—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
    • B64G1/645—Separators
    • B64G1/6459—Fluid-actuated
    • 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)
  • Testing Of Engines (AREA)

Abstract

PURPOSE: To easily separate an auxiliary booster in a rocket having a separable auxiliary booster by providing a separating device to generate asymmetric pneumatic force to a frame axis of a rocket main body only at the time of separating the auxiliary booster. CONSTITUTION: A rocket main body 1 is separably provided with an auxiliary booster 2 to be symmetric to its frame axis. The auxiliary booster 2 is provided with a separating device 3 having a cross section of a rhomboid form, for example. At this time, at the time of normal flight of the rocket main body 1, that is when the auxiliary booster 2 is not separated, the separating device 3 is stored in the auxiliary booster 2, or a reference surface passing a vertical vertex of the rhomboid form is set to be parallel to a frame axis of the rocket main body 1. At the time of separating the auxiliary booster 2, the reference surface of the separating device is set to generate a specified angle to the frame axis of the rocket main body 1. Pneumatic force perpendicular to flow is thus generated, thereby the rocket main body 1 and the auxiliary booster 2 can be easily separated from each other.
JP62237092A 1987-09-24 1987-09-24 Rocket with auxiliary booster separator Pending JPS6483500A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62237092A JPS6483500A (en) 1987-09-24 1987-09-24 Rocket with auxiliary booster separator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62237092A JPS6483500A (en) 1987-09-24 1987-09-24 Rocket with auxiliary booster separator

Publications (1)

Publication Number Publication Date
JPS6483500A true JPS6483500A (en) 1989-03-29

Family

ID=17010290

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62237092A Pending JPS6483500A (en) 1987-09-24 1987-09-24 Rocket with auxiliary booster separator

Country Status (1)

Country Link
JP (1) JPS6483500A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007260670A (en) * 2006-03-03 2007-10-11 Daiki Ataka Engineering Co Ltd Construction method of organic waste treatment facility

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007260670A (en) * 2006-03-03 2007-10-11 Daiki Ataka Engineering Co Ltd Construction method of organic waste treatment facility

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