Results 111 to 120 of about 13,180 (230)
MachinesLiquid rocket engines occasionally experience abnormal phenomena with unclear mechanisms, causing difficulty in design improvements. To address the above issue, a data mining method that combines ante hoc explainability, post hoc explainability, and ...
Xiaopu Zhang, Wubing Miao, Guodong Liu
doaj +1 more source
Metal-organic frameworks as hypergolic additives for hybrid rockets. [PDF]
Chem Sci, 2022 Jobin O +8 more
europepmc +1 more source
Advanced Earth-to-orbit propulsion technology program overview: Impact of civil space technology initiative [PDF]
The NASA Earth-to-Orbit (ETO) Propulsion Technology Program is dedicated to advancing rocket engine technologies for the development of fully reusable engine systems that will enable space transportation systems to achieve low cost, routine access to ...
Stephenson, Frank W., Jr.
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Numerical simulation of long and slender cylinders vibrating in axial flow applied to the Myrrha reactor [PDF]
, 2012 Flow induced vibrations are an important concern in the design of nuclear reactors. One of the possible designs of the 4th generation nuclear reactors is a lead-cooled fast reactor of which MYYRHA is a prototype.
De Ridder, Jeroen +3 more
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H2 fueled flightweight ramjet construction and test [PDF]
The ACES Program began the investigation of regeneratively cooled ramjet engines for propelling aircraft at Mach 6 to 8 flight regimes while collecting and processing air for later use as oxidizer in rocket propulsion into an orbit flight mode.
Malek, Albert
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Hybrid holographic non-destructive test system [PDF]
, 1978 An automatic hybrid holographic non-destructive testing (HNDT) method and system capable of detecting flaws or debonds contained within certain materials are described.
Kurtz, R. L.
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Swirl Injection Effects on Hybrid Rocket Motors
Journal of Aerospace Technology and Management, 2015 In the last decades, hybrid rocket engines have been increasingly studied and used in space vehicles. However, the low regression rates and specific impulses still represent major drawbacks to this technology. The objective of this study was to quantify
Susane Ribeiro Gomes +2 more
doaj
Analysis of carbon nano particle variant as the propellant fuel to increase specific impulses of rockets. [PDF]
F1000Res, 2023 Navalino R, Muda N, Hafizah M, Ruyat Y.
europepmc +1 more source
Launch vehicle performance using metallized propellants [PDF]
Metallized propellant propulsion systems are considered as replacements for the solid rocket boosters and liquid sustainer stages on the current launch vehicles: both the Space Transportation System (STS) and the Titan 4.
Palaszewski, Bryan A., Powell, Richard
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Space Transportation Materials and Structures Technology Workshop [PDF]
The Space Transportation Materials and Structures Technology Workshop was held on September 23-26, 1991, in Newport News, Virginia. The workshop, sponsored by the NASA Office of Space Flight and the NASA Office of Aeronautics and Space Technology, was ...
Cazier, Frank W., Jr., Gardner, James E.
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