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基本信息

【范围】

This SAE Aerospace Information Report (AIR) presents information on gas energy limited propulsion engine starting systems employed in commercial and military applications and remote industrial sites. The types of systems discussed utilize solid propellant cartridge gas, monopropellant hydrazine gas, bipropellant gas, compressed stored gas, and cryogenic stored nitrogen. Presented information conveys design features, performance capabilities and system limitations with methods of computing results.strRefField

【与前一版的变化】

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包含图表

FIGURE 1 - Basic Com	r	w
GHP	HAD	γ
Pc	HAD	FIGURE 2 - Schematic
FIGURE 3 - Schematic	FIGURE 4 - Schematic	TABLE 1 - Hydrazine-
n2h4	HAD	TABLE 2 - Monofuel P
HAD	GHP	FIGURE 6 - Typical P
FIGURE 7 - Typical G	TABLE 3	Specific Power
FIGURE 8 - Schematic	(Eq. 8)	(Eq.
(Eq. 9	FIGURE 9A - Compress	FIGURE 9B - Compress
FIGURE 10 - Temperat	FIGURE 11 - Cryogeni	FIGURE 12 - Schemati
(Eq. 11	(Eq. 12	TABLE 4 - Typical Pe
(Eq.	FIGURE 1 - Basic Com	(Eq. 1
(Eq. 2	(Eq. 2	(Eq. 3
(Eq. 4	FIGURE 2 - Schematic	FIGURE 3 - Schematic