Spacecraft attitude impacts on COLD-SAT non-vacuum jacketed LH2 supply tank thermal performance [PDF]
The Cryogenic On-Orbit Liquid Depot - Storage, Acquisition and Transfer (COLD-SAT) spacecraft will be launched into low earth orbit to perform fluid management experiments on the behavior of subcritical liquid hydrogen (LH2).
Arif, Hugh
core +1 more source
Large diameter astromast development, phase 1 [PDF]
Coilable-longeron lattice columns called Astromasts (trademark) were manufactured for a variety of spacecraft missions. These flight structures varied in diameter from 0.2 to 0.5 meter (9 to 19 in.), and the longest Astromast of this type deploys to a ...
Finley, L. A. +2 more
core +1 more source
The Effect of Tropical Environment on Fatigue Failure in Royal Malaysian Airforce (RMAF) Aircraft Structure and Operational Readiness. [PDF]
Venugopal A +4 more
europepmc +1 more source
Wire Arc Additive Manufacturing (WAAM) for Aluminum-Lithium Alloys: A Review. [PDF]
Rodríguez-González P +2 more
europepmc +1 more source
A Comprehensive Review of Friction Stir Additive Manufacturing (FSAM) of Non-Ferrous Alloys. [PDF]
Hassan A +3 more
europepmc +1 more source
Space station structures and dynamics test program [PDF]
The design, construction, and operation of a low-Earth orbit space station poses challenges for development and implementation of technology. One specific challenge is the development of a dynamics test program for defining the space station design ...
Bugg, Frank M. +3 more
core +1 more source
Corrosion Resistance of Aluminum Alloy AA2024 with Hard Anodizing in Sulfuric Acid-Free Solution. [PDF]
Miramontes JC +10 more
europepmc +1 more source
Motion synchronization of a mechanism to deploy and restow a truss beam [PDF]
The functions of the Control of Flexible Structures I (COFS I) deployer and retractor assembly (DRA) are primarily to deploy and retract the Mast I beam, and secondarily to latch, unlatch, and restow the DRA mechanism.
Lucy, M.
core +1 more source
Fatigue analysis of mini-mast space truss [PDF]
The functional, structural adequacy of a 20 meter long generic space truss (Mini-Mast), subjected to fatigue loading, was examined with respect to the failure modes which are most likely to occur during services.
Hwang, Shoi Y.
core +1 more source
Structure Life Extension towards the Structural Integrity of Sukhoi Su-30MKM. [PDF]
Venugopal A +5 more
europepmc +1 more source

