Aerothermodynamic overview, X-34

被引：4

作者：

Fuhrmann, HD ^{[1
]}

Hildebrand, J ^{[1
]}

Lalicata, T ^{[1
]}

机构：

[1] Orbital Sci Corp, Dulles, VA 20166 USA

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1999年 / 36卷 / 02期

关键词：

D O I：

10.2514/2.3437

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The X-34 is a reusable launch vehicle (RLV) technology demonstrator developed by Orbital Sciences Corporation (OSC) for NASA's RLV program. Throughout the development, NASA and OSC balanced technical risk, schedule, and cost in all areas. With the application of the latest in Computational Fluid Dynamics, experimental, and engineering methods, the resulting design is sufficiently optimized to meet the goals of the X-34 program.

引用

页码：153 / 159

页数：7

共 50 条

[1] X-34 is on the Fastrac
不详
AEROSPACE ENGINEERING, 1999, 19 (12) : 32 - 32
[2] X-34 tank
不详
AVIATION WEEK & SPACE TECHNOLOGY, 2000, 152 (07): : 17 - 17
[3] X-34 is on the Fastrac
Bokulich, F
AEROSPACE ENGINEERING, 1999, 19 (05) : 19 - 19
[4] X-34 designs locked in
Anselmo, JC
AVIATION WEEK & SPACE TECHNOLOGY, 1997, 146 (23): : 33 - 33
[5] X-34 designs locked in
Aviation Week and Space Technology (New York), 1997, 146 (23):
[6] X－34计划压缩规模
中国航天, 1996, (09) : 41 - 41
[7] Computational aeroheating predictions for X-34
Kleb, William L.
Wood, William A.
Gnoffo, Peter A.
Alter, Stephen J.
Journal of Spacecraft and Rockets, 36 (02): : 179 - 188
[8] DC DETRACTOR HELPS X-34
BYRD, RJ
AVIATION WEEK & SPACE TECHNOLOGY, 1995, 142 (20): : 8 - 8
[9] NASA suspends X-34 booster
Aviation Week and Space Technology (New York), 1995, 143 (19):
[10] Computational aeroheating predictions for X-34
Kleb, WL
Wood, WA
Gnoffo, PA
Alter, SJ
JOURNAL OF SPACECRAFT AND ROCKETS, 1999, 36 (02) : 179 - 188

← 1 2 3 4 5 →