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RL10
Known as:
RLS ES 10
Provider: Reliance Life Sciences, Mumbai, India. No information from provider. This cell line meets the criteria for the use of human embryonic stem…
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National Institutes of Health
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Papers overview
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2014
2014
RL10 Engine Ability to Transition from Atlas to Shuttle/Centaur Program
Joseph F. Baumeister
2014
Corpus ID: 111275061
A key launch vehicle design feature is the ability to take advantage of new technologies while minimizing expensive and time…
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Review
2010
Review
2010
Throttling Characteristics of the RL10 Derivative Common Extensible Cryogenic Engine -- Demo 1.6 and 1.7 Test Results
M. Devine
,
J. Hulka
,
Walter M. Adamski
,
Corey D. Brown
2010
Corpus ID: 107704497
The Common Extensible Cryogenic Engine (CECE) is a deep throttling cryogenic Lunar Module Descent Engine (LMDE) technology…
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2008
2008
Rice plant type relevant gene RL10 and use thereof
严长杰
,
程祝宽
,
顾铭洪
2008
Corpus ID: 140322031
The invention belongs to the field of genetics and breeding, in particular relates to a rice plant type related gene RL10 and…
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2005
2005
Small Broadband Antenna Designs for 3G Handset Applications
Z. Rashid
,
J. L. Hui
,
Ng Kok Jiunn
2005
Corpus ID: 59140134
Dua reka bentuk antena set tangan yang diperbaiki, kecil, padat dan berjalur lebar bagi jalur 3G berdasarkan kaedah tompok…
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1999
1999
Expression of protein tyrosine phosphatase PTP‐RL10 and its isoform in the mouse testis
H. Tokuchi
,
H. Higashitsuji
,
+6 authors
J. Fujita
International journal of urology
1999
Corpus ID: 38524556
Background : The cytoplasmic‐type protein tyrosine phosphatase PTP‐RL10/PTPD1/PTP2E contains an ezrin‐like domain and associates…
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1991
1991
Cryogenic upper stage propulsion: RL10 and derivative engines
J. R. Brown
1991
Corpus ID: 107157496
The capabilities and characteristics of the RL10 rocket engine are examined. The engine model history is presented. The RL10…
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1989
1989
Design and analysis report for the flight weight 20-inch Columbium secondary nozzle for the RL10 engine
J. Castro
1989
Corpus ID: 92901737
Pratt & Whitney (P and W) is currently under contract to NASA-LeRC for a multi-year program to evaluate the feasibility of the…
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1988
1988
Breadboard RL10-2B low-thrust operating mode (second iteration) test report
P. Kanic
,
Raymond B. Kaldor
,
P. Watkins
1988
Corpus ID: 106959673
Cryogenic rocket engines requiring a cooling process to thermally condition the engine to operating temperature can be made more…
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1987
1987
Breadboard RL10-11B low thrust operating mode
T. Kmiec
,
D. Galler
1987
Corpus ID: 106895277
Cryogenic space engines require a cooling process to condition engine hardware to operating temperature before start. This can be…
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1966
1966
Adaptation of the RL10 engine for fluorine- hydrogen application.
T. E. Bailey
1966
Corpus ID: 93961834
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