LOX / LNG ENGINE DESIGN AND TEST RESULTS FOR J-II ROCKET

LOX / LNG ENGINE DESIGN AND TEST RESULTS FOR J-II ROCKET

Author(s):

Ishikawa, Y. ( Ishikawajima-Harima Heavy Industries Co., Ltd. )

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Ser. no.:

2000

Pub. Year:

2000

No.:

2000-3454

Paper no.:

00-3454

Page(from):

1

Page(to):

7

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050879
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	36th
Conf. info. (Venue):	Huntsville, AL
Conf. info. (Date):	2000.07.16-2000.07.19
Note for article:	36 th AIAA / ASME / SAE / ASEE Joint Propulsion Conference and Exhibit 16 - 19 July 2000 Huntsville, Alabama

Similar Items:

1 Technical Paper Current Study Status of the Advanced Technologies for the J-I Upgrade Launch Vehicle -LOX/LNG Engine- Torano,Y., Arita,M., Takahashi,H., Higashino,K., Ishii,M., Ikeda,H. American Institute of Aeronautics and Astronautics	7 Technical Paper Design and Operational Aspect of LOX/LH2 Propulsion System of Reusable Vehicle Testing (RVT) Naruo,Yoshihiro, Tokudome,Shin-ichiro, Ishii,Masahiro, Higashino,Kazuyuki American Institute of Aeronautics and Astronautics
2 Technical Paper Fundamental Study on Coking Characteristics of LNG Rocket Engines K. Higashino, M. Sugioka, T. Kobayashi, R. Minato, Y. Maru, Y. Sasayama, M. Otsuka, T. Makino, H. Sakaguchi American Institute of Aeronautics and Astronautics	8 Technical Paper An Application of Commercial Grade Hydrogen Peroxide for Hybrid/Liquid Rocket Engine (II) Tsujikado, N., Koshimae, M., Ishikawa, R., Kitahara, K., Ishihara, A. American Institute of Aeronautics and Astronautics
3 Technical Paper Hot Firing Tests of Liquid Rocket Engine Using LOX/LNG Cho, Y., Chang, H. American Institute of Aeronautics and Astronautics	9 Technical Paper Recent Advances on LOX/Methane Combustion for Liquid Rocket Engine Injector. Zurbach, S., Thomas, J.L., Vuillermoz, P., Vingert, L., Habibllah, M. American Institute of Aeronautics and Astronautics
4 Technical Paper High Area Ratio LOX-Augmented Nuclear Thermal Rocket (LANTR) Testing Bulman,M.J., Messitt,D.G., Neill,T.M., Borowski,S.K. American Institute of Aeronautics and Astronautics	10 Technical Paper TRW LCPE 650 KLBf LOX/LH2 Test Results Gavitt, K., Mueller, T., Wong, T., Thom, H., Murphy, C., Weede, J. American Institute of Aeronautics and Astronautics
5 Technical Paper Continued Lox-Augmented Nuclear Thermal Rocket (LANTR) Testing. Bulman, M.J., Messitt, D.G., Neill, T.M., Borowski, S.K. American Institute of Aeronautics and Astronautics	11 Technical Paper The Effect of Injector and Intake Port Design on In-Cylinder Fuel Droplet Distribution, Airflow and Lean Burn Performance for a Honda VTEC-E Engine Carabateas, N. E., Taylor, A. M. K. P., Whitelaw, J. H., Ishii, Kiyoshi, Yoshida, Kazuo, Matsuki, Massato Society of Automotive Engineers
6 Technical Paper Testing Results of Critical Elements for Reusable Rocket Engine M. Yoshida, S. Takada, Y. Naruo, K. Niu American Institute of Aeronautics and Astronautics	12 Technical Paper Development of 'Chase 10' Liquid Rocket Engine having 10tf thrust using lox & lng (methane) K. Kim, D. Ju American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12