GB1416342A - Fixed-wing dual-purpose aeroplanes - Google Patents

Fixed-wing dual-purpose aeroplanes

Info

Publication number
GB1416342A
GB1416342A GB528872A GB528872A GB1416342A GB 1416342 A GB1416342 A GB 1416342A GB 528872 A GB528872 A GB 528872A GB 528872 A GB528872 A GB 528872A GB 1416342 A GB1416342 A GB 1416342A
Authority
GB
United Kingdom
Prior art keywords
wings
portions
feb
planar
leading edge
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
Application number
GB528872A
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.)
Senhenn L A
Original Assignee
Senhenn L A
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 Senhenn L A filed Critical Senhenn L A
Priority to GB528872A priority Critical patent/GB1416342A/en
Publication of GB1416342A publication Critical patent/GB1416342A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/14—Space shuttles

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Transmission Devices (AREA)

Abstract

1416342 Aircraft wings; space shuttles L A SENHENN 5 Feb 1973 [4 Feb 1972] 5288/72 Headings B7G and B7W An aircraft intended for use as a space shuttle comprises a fuselage 10 which carries foreplanes 11 and extends from a conical nose portion into an aft portion which carries main wings 12 and houses a plurality of rocket propulsion units 15 and braking propulsion units enclosed by covers 25. There are dorsal and ventral fins 21, 22, stub tail planes 23, 24, nacelles 16 housing main undercarriage units 17, a nacelle 20 for a front undercarriage unit and a cockpit 19. The wings are planar and wings 11 have an adjustable leading edge portion 29, the wings 12 having similar portions 34, 35. For vertical rocket-propelled ascent the leading edge portions are planar with their respective wings but during re-entry through the atmosphere the portions 29 are hinged upwardly and portions 34, 35 are hinged downwardly to give respectively a positive and negative pitching moment.
GB528872A 1972-02-04 1972-02-04 Fixed-wing dual-purpose aeroplanes Expired GB1416342A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB528872A GB1416342A (en) 1972-02-04 1972-02-04 Fixed-wing dual-purpose aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB528872A GB1416342A (en) 1972-02-04 1972-02-04 Fixed-wing dual-purpose aeroplanes

Publications (1)

Publication Number Publication Date
GB1416342A true GB1416342A (en) 1975-12-03

Family

ID=9793304

Family Applications (1)

Application Number Title Priority Date Filing Date
GB528872A Expired GB1416342A (en) 1972-02-04 1972-02-04 Fixed-wing dual-purpose aeroplanes

Country Status (1)

Country Link
GB (1) GB1416342A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110775296A (en) * 2019-11-12 2020-02-11 中国空气动力研究与发展中心计算空气动力研究所 Design method for pressure center backward movement of reusable aerospace vehicle
CN113562160A (en) * 2021-08-07 2021-10-29 中国航空工业集团公司沈阳飞机设计研究所 Front wing application method for improving pitching moment characteristic of airplane
CN114379765A (en) * 2021-12-30 2022-04-22 中电科芜湖通用航空产业技术研究院有限公司 Unmanned aerial vehicle's front wing and unmanned aerial vehicle

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110775296A (en) * 2019-11-12 2020-02-11 中国空气动力研究与发展中心计算空气动力研究所 Design method for pressure center backward movement of reusable aerospace vehicle
CN113562160A (en) * 2021-08-07 2021-10-29 中国航空工业集团公司沈阳飞机设计研究所 Front wing application method for improving pitching moment characteristic of airplane
CN113562160B (en) * 2021-08-07 2024-01-02 中国航空工业集团公司沈阳飞机设计研究所 Front wing application method for improving pitching moment characteristics of airplane
CN114379765A (en) * 2021-12-30 2022-04-22 中电科芜湖通用航空产业技术研究院有限公司 Unmanned aerial vehicle's front wing and unmanned aerial vehicle

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Legal Events

Date Code Title Description
CSNS Application of which complete specification have been accepted and published, but patent is not sealed