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10 results

Technical Paper

1. AN EXPERIMENTAL STUDY ON A 14 kN LINEAR AEROSPIKE-NOZZLE COMBUSTOR

Sakamoto, H. ; Takahashi, M. ; Sasaki, M. ; Tomita, T. ; Kusaka, K. ; Tamura, H.

Pub. info.:	AIAA paper. pp.1-8, 1999. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1999

Technical Paper

2. Experimental study on combustion stability characteristics of non-swirl coaxial injectors

Sasaki, M. ; Sakamoto, H. ; Takahashi, M. ; Tomita, T. ; Tamura, H.

Pub. info.:	AIAA paper. pp.1-8, 1998. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1998

Technical Paper

3. An experimental study on a 14 kN linear aerospike-nozzle combustor

Sakamoto, H. ; Takahashi, M. ; Sasaki, M. ; Tomita, T. ; Kusaka, K. ; Tamura, H.

Pub. info.:	AIAA paper. pp.1-8, 1999. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1999

Technical Paper

4. Comparative study of recessed and non-recessed swirl coaxial injectors

Sasaki, M. ; Sakamoto, H. ; Takahashi, M. ; Tomita, T. ; Tamura, H.

Pub. info.:	AIAA paper. pp.1-7, 1997. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1997

Technical Paper

5. LOX/LH2 subscale swirl coaxial injector testing

Tamura, H. ; Sakamoto, H. ; Takahashi, M. ; Sasaki, M. ; Tomita, T. ; Nagao, R.

Pub. info.:	AIAA paper. pp.1-6, 1997. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1997

Technical Paper

6. Experimental Evaluation of Side-Load Characteristics on TP, CTP and TO Nozzles

Tomita, T. ; Sakamoto, H. ; Onodera, T. ; Sasaki, M. ; Takahashi, M. ; Watanabe, Y.

Pub. info.:	AIAA meeting papers on disc. 2004. [Reston, Va.]. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	40th

Technical Paper

7. Obserbation of Lox/Hydrogen Combustion Flame in a Rocket Chamber During Chugging Instability

Tamura, H. ; Sakamoto, H. ; Takahashi, M. ; Sasaki, M. ; Onodera, T.

Pub. info.:	AIAA paper. 2003. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	2003

Technical Paper

8. Reduction of Combustion Pressure Fluctuations in Rocket Engine

Onodera, T. ; Sakamoto, H. ; Takahashi, M. ; Sasaki, M. ; Tamura, H.

Pub. info.:	AIAA paper. 2003. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	2003

Technical Paper

9. Sub-Scale Nozzle Combustion Tests of the LE-7A Engine for Clarification of Large Side-Load (I) Formation of RSS Structure Due to Combustion Condition.

Tomita, T. ; Sakamoto, H. ; Takahashi, M. ; Sasaki, M. ; Tamura, H.

Pub. info.:	AIAA paper. 2002. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	2002

10.

Technical Paper

10. Sub-scale Nozzle Combustion Tests of the LE-7A Engine for Clarification of Large Side-Load (II) Influence of a Step in Nozzle Contour on Side-Ioad.

Tomita, T. ; Sakamoto, H. ; Takahashi, M. ; Sasaki, M. ; Tamura, H.

Pub. info.:	AIAA paper. 2002. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	2002

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