Investigation of Two-Stage-to-Orbit Air-Breathing Launch Vehicle Configurations

Investigation of Two-Stage-to-Orbit Air-Breathing Launch Vehicle Configurations

著者名:

Dissel, A. ( Astrox Corporation, College Park, MD )
Kothari, A.
Lewis, M. ( University of Maryland, College Park, MD )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : International Space Planes and Hypersonic Systems and Technologies Conference

シリーズ巻号:

13th

発行年:

2005

通号:

2005-3244

ペーパー番号:

AIAA Paper 2005-3244

出版情報:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200508 [CD-ROM 2005 Disc 8]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001623
シリーズID:	PA00000152
会議名:	AIAA/CIRA International Space Planes and Hypersonics Systems and Technologies Conference
回次:	13th
会議開催地:	Capua, Italy
会議開催年:	2005.05.16-2005.05.20

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1 テクニカルペーパー Weight Growth Study of Reusable Launch Vehicle Systems Dissel, A., Kothari, A., Lewis, M. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Generalized Vehicle Performance Closure Model for Two-Stage-to-Orbit Launch Vehicles Qu, M., Sohn,J., Gage,P., Bradford,J., Starr,B. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー System Analysis of Launch Transportation Options for Crew Exploration Vehicle Dissel, A., Kothari, A., Raghavan, V., Lewis, M. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Two-Stage-to-Orbit Reusable Launch Vehicle Propulsion Performance Study Brock, M., Franke, M. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Quicksat: A Two Stage to Orbit Reusable Launch Vehicle Utilizing Air Breathing Propulsion for Responsive Space Access Eklund, D. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Weight Analysis of Two-Stage-To-Orbit Reusable Launch Vehicles Caldwell, R., Franke, M., Eklund, D. American Institute of Aeronautics and Astronautics
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6 テクニカルペーパー Comparison of HTHL and VTHL Airbreathing and Rocket Systems for Access to Space Dissel, A., Kothari, A., Raghavan, V., Lewis, M. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー CONCEPTUAL DESIGN OF TWO-STAGE-TO-ORBIT HYBRID LAUNCH VEHICLE CASE WESTERN RESERVE UNIVERSITY National Aeronautics and Space Adminstration

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