Works matching IS 05493811 AND DT 2016 AND VI 59 AND IP 6
Results: 9
Dissociation Rate Coefficient of Oxygen for O<sub>2</sub> + O Reaction.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Science, 2016, v. 59, n. 6, p. 371, doi. 10.2322/tjsass.59.371
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- Publication type:
- Article
Abstracts of the Papers Published in Journal of the Japan Society for Aeronautical and Space Sciences (Vol. 64, No. 5, Oct. 2016).
- Published in:
- 2016
- Publication type:
- Abstract
Conservation-Law Approach for Transition in Pipe Flows.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Science, 2016, v. 59, n. 6, p. 356, doi. 10.2322/tjsass.59.356
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- Publication type:
- Article
Deployment Control of a Tethered Satellite System for Rendezvous with a Target.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Science, 2016, v. 59, n. 6, p. 313, doi. 10.2322/tjsass.59.313
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- Publication type:
- Article
Comparing Aerial-Deployment-Mechanism Designs for Mars Airplane.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Science, 2016, v. 59, n. 6, p. 323, doi. 10.2322/tjsass.59.323
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- Publication type:
- Article
Estimation of the Highest Surface Temperature for CFRP Ablator by Raman Analysis.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Science, 2016, v. 59, n. 6, p. 364, doi. 10.2322/tjsass.59.364
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- Publication type:
- Article
Supersonic Inlet Control Design for Integrated Aero Propulsion during Supersonic Cruising State.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Science, 2016, v. 59, n. 6, p. 349, doi. 10.2322/tjsass.59.349
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- Publication type:
- Article
Fundamental Design Optimization of an Innovative Supersonic Transport Configuration and Its Design Knowledge Extraction.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Science, 2016, v. 59, n. 6, p. 340, doi. 10.2322/tjsass.59.340
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- Publication type:
- Article
Radiative Heating in Combustion Chamber of Liquid Propellant Rocket Engines.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Science, 2016, v. 59, n. 6, p. 332, doi. 10.2322/tjsass.59.332
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- Publication type:
- Article