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Aerospike Database
Known as:
Aerospike
Aerospike is a flash-optimized in-memory open source NoSQL database and the name of the company that produces it.
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16 relations
Ansible
Apache Cassandra
Comparison of structured storage software
Distributed cache
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Broader (1)
NoSQL
Papers overview
Semantic Scholar uses AI to extract papers important to this topic.
2018
2018
Chapter Six - NoSQL Hands On
Rebika Rai
,
Prashant Chettri
Advances in Computing
2018
Corpus ID: 64902224
2018
2018
Polypus: a Big Data Self-Deployable Architecture for Microblogging Text Extraction and Real-Time Sentiment Analysis
Rodrigo Martínez-Castaño
,
J. C. Pichel
,
Pablo Gamallo
arXiv.org
2018
Corpus ID: 42084104
In this paper we propose a new parallel architecture based on Big Data technologies for real-time sentiment analysis on…
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2016
2016
Fuel Manifold Fuel Feed Line Detonation Channel Exhaust Exhaust Aerospike Plug Nozzle Channel Width Fuel Truncated Plug Nozzle Air Fuel Exhaust Exhaust
M. Fotia
,
J. Hoke
2016
Corpus ID: 174769310
Rotating detonation engines have shown promise as a potential avenue to integrate pressure-gain combustion into aerospace…
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2015
2015
Implementing Ultra Low Latency Data Center Services with Programmable Logic
J. Lockwood
,
M. Monga
IEEE 23rd Annual Symposium on High-Performance…
2015
Corpus ID: 7468241
Data centers require many low-level network services to implement high-level applications. Key-Value Store (KVS) is a critical…
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2013
2013
Flow Visualizations of A Simplified Linear Aerospike Model Using Background Oriented Schlieren
Hidemi Takahashi
,
S. Tomioka
,
N. Sakuranaka
,
T. Tomita
,
Kohei Kuwamori
,
G. Masuya
2013
Corpus ID: 61765963
Flow interaction between external flow and cell jet flows of a simplified clustered linear aerospike model was experimentally…
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2012
2012
Computational Design of Upperstage Chamber, Aerospike, and Cooling Jacket for Dual-Expander Rocket Engine
David Martin
2012
Corpus ID: 107974955
Abstract : To increase the performance of the current US satellite launch capability, new rocket designs must be undertaken. One…
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2011
2011
Design and Analysis of a Reusable N2O-Cooled Aerospike Nozzle for Labscale Hybrid Rocket Motor Testing
D. Grieb
,
P. Lemieux
,
W. R. Murray
,
J. Mello
,
Terry H. Cooke
,
J. A. Gerhardt
2011
Corpus ID: 110357470
A reusable oxidizer-cooled annular aerospike nozzle was designed for testing on a labscale PMMA-N2O hybrid rocket motor at the…
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2004
2004
Flow Visualization of Flowfield Structures around an Aerospike Nozzle using LIF and PSP
T. Niimi
,
H. Mori
,
M. Taniguchi
2004
Corpus ID: 109618224
Aerospike nozzles have been expected to be used for an engine of a reusable space shuttle to respond to growing demand for rocket…
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Highly Cited
2002
Highly Cited
2002
Influence of a Counterflow Plasma Jet on Supersonic Blunt-Body Pressures
V. Fomin
,
A. Maslov
,
+5 authors
G. A. Pozdnyakov
2002
Corpus ID: 115133753
Aerodynamic augmentation in the presence of a thin high-temperature onboard plasma jet directed upstream of a slightly blunted…
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2001
2001
Analysis of X-33 Linear Aerospike Plume Induced Base-Heating Environment During Power-Pack Out
Ten-See Wang
,
Robert Williams
,
+4 authors
J. Turner
2001
Corpus ID: 106948419
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