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Liquid Propellant Gas Generation Systems
- Aerospace Standard
- AIR1343B
- Stabilized
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This information report presents a preliminary discussion of liquid propellant gas generation (LPGG) systems. A LPGG system, as used herein, is defined as a system which stores a liquid propellant and, on command, discharges and converts the liquid propellant to a gas. The LPGG system can interface with a gas-to-mechanical energy conversion device to make up an auxiliary power system. Figure 1 shows a block diagram of LPGG system components which include a propellant tank, propellant expulsion system, propellant control and a decomposition (or combustion) chamber.
The purpose of this report is to provide general information on the variety of components and system arrangements which can be considered in LPGG design, summarize advantages and disadvantages of various approaches and provide basic sizing methods suitable for initial tradeoff purposes.
Rationale
This document has been determined to contain basic and stable technology which is not dynamic in nature.
Recommended Content
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
TABLE 1 | Monopropellant Characteristics Viscosity, 77 °F (25 °C) | |
TABLE 2 | Constituents of Hydrazine Blends With Depressed Freezing Points | |
TABLE 3 | Physical and Chemical Properties of Hydrazine Monopropellants | |
TABLE 4 | Typical Bipropellant Characteristics | |
TABLE 5 | Characteristics of Typical Propellant |
Issuing Committee
A6C4 is responsible for the development of standards, processes, and practices related to Fluid Power Sources (Pumps, Motors, Accumulators), and the integration of these components for Commercial and Military air vehicles. The panel provides a forum for government engineers, prime contractors, and suppliers to exchange technical information, regulatory updates, recent technology developments, issues related to system development and in service operation and lessons learned.
Reference
Number | Title |
---|---|
AF/SSD-TR-61-6 | This document is not part of the subscrption. |
AFRPL-TR-67-219 | This document is not part of the subscrption. |
AFRPL-TR-69-149 | This document is not part of the subscrption. |
AIAA Paper No. 70-606 | This document is not part of the subscrption. |
AIAAPaperNo.70- | This document is not part of the subscrption. |
F04611-69-C-000 | This document is not part of the subscrption. |
F04611-69-C-0005 | This document is not part of the subscrption. |
NASA Contract NAS7-372 | This document is not part of the subscrption. |
NASA Contract NAS7-388 | This document is not part of the subscrption. |
NASAContractNAS | This document is not part of the subscrption. |
NASASP-8081 | This document is not part of the subscrption. |
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