RAM ACCELERATOR DIRECT SPACE LAUNCH SYSTEM - NEW CONCEPTS

被引:22
作者
BOGDANOFF, DW [1 ]
机构
[1] ELORET INST,PALO ALTO,CA 94303
关键词
D O I
10.2514/3.23502
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The ram accelerator, a chemically driven ramjet-in-tube device is a new option for direct launch of acceleration-insensitive payloads into Earth orbit. The projectile is the centerbody of a ramjet and travels through a tube filled with a premixed fuel-oxidizer mixture. The tube acts as the cowl of the ramjet. A number of new concepts for a ram accelerator space launch system are presented. The velocity and acceleration capabilities of a number of ram accelerator drive modes, including several new modes, are given. Passive (fin) stabilization during atmospheric transit is investigated and found to be promising. Gasdynamic heating in-tube and during atmospheric transit is studied; the former is found to be severe, but may be alleviated by the selection of the most suitable drive modes, transpiration cooling, or a hydrogen gas core in the launch tube. To place the payload in Earth orbit, scenarios using one impulse and three impulses (with an aeropass) and a new scenario involving an auxiliary vehicle are studied. The auxiliary vehicle scenario is found to be competitive regarding payload, and requires a much simpler projectile, but has the disadvantage of requiring the auxiliary vehicle.
引用
收藏
页码:481 / 490
页数:10
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