Deployment/retraction mechanism for solar maximum mission high gain antenna system [PDF]
, 1979 A mechanism called a deployment/retraction assembly (DRA) which provides not only a stable, but a deployable platform for the high gain antenna system (HGAS) aboard the Solar Maximum Mission (SMM) spacecraft is described.
Bennett, N., Preiswerk, P.
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MATEC Web of Conferences, 2017 Space deployable mast is an important device or system, which can deploy and support spacecraft fittings on orbit, such as payload, solar array, antenna, and etc.
Luo Hai-jun +3 more
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Hoop/column antenna deployment mechanism overview [PDF]
, 1985 The hoop/column antenna program is directed toward the development of a cost effective, large area, self deploying reflector antenna system. Large surface area antenna systems are required in future space missions involving improved land communications ...
Allen, B. B., Butler, D. H.
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Numerical-experimental static analysis of the effort of the crossbar-longeron in the semi-trailer frame [PDF]
AIP Conference Proceedings, 2019 The article presents the verification process of a new type of transverse of beam semi-trailer main frame, as an element of the process of developing a new structural design. The main goal of the research was to determine the possibility of using bent sheet metal profiles as the transverse beams in the curtain semi-trailer frame.
openaire +1 more source
CALCULATION AND DESIGN PROCEDURE OF VIBRO-SHOCK HARDENING BED GUARD FOR LONG PIECES
Вестник Донского государственного технического университета, 2018 The noise enclosure design for the vibro - shock har dening bed of the helicopter longerons is considered. The noise abatement performance in the operating space is shown.
Mikhail E. Popov, Victor P. Zharov
doaj
CALCULATION AND DESIGN PROCEDURE OF VIBRO-SHOCK HARDENING BED GUARD FOR LONG PIECES
Advanced Engineering Research, 2012 The noise enclosure design for the vibro - shock har dening bed of the helicopter longerons is considered. The noise abatement performance in the operating space is shown.
Mikhail E. Popov, Victor P. Zharov
doaj
Multiaxial fatigue of in-service aluminium longerons for helicopter rotor-blades
Fracture and Structural Integrity, 2018 Fatigue cracking of longerons manufactured from Al-alloy AVT-1 for helicopter in-service rotor-blades was considered and crack growth period and equivalent of tensile stress for different blade sections were estimated.
A. Shanyavskiy, A. Toushentsov
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Securing mechanism for the deployable column of the Hoop/Column antenna [PDF]
, 1983 The Column Longeron Latch (CLL) was designed and developed as the securing mechanism for the deployable, telescoping column of the Hoop/Column antenna. The column is an open lattice structure with three longerons as the principal load-bearing members. It
Ahl, E. L., Jr.
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THEORETICAL STUDY ON VIBROACOUSTICS UNDER DYNAMIC TEST FOR CYCLICAL STRENGTH
Вестник Донского государственного технического университета, 2018 The theoretical study on the excitation of the equipment vibrations and noise emission under the dynamic testing of helicopter longerons is resulted. The dependences for determining vibration spectra in the operating space are obtained.
Sergey A. Shamshura +2 more
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Design, development and mechanization of a precision deployable truss with optimized structural efficiency for spaceborne applications [PDF]
, 1982 A deployable mast concept which meets the weight, size and stability requirements for a feed support structure for offset antennas up to 100 meters in diameter is discussed.
Craighead, N. D. +2 more
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