An analysis of the combustion products resulting from the solid propellant rocket engines of the space shuttle booster is presented. Calculation of the degree of pollution indicates that the only potentially harmful pollutants, carbon monoxide and hydrochloric acid, will be too diluted to constitute a hazard. The mass of products ejected during a launch within the troposphere is insignificant in terms of similar materials that enter the atmosphere from other sources. Noise pollution will not exceed that obtained from the Saturn 5 launch vehicle
An analysis of the water entry loads imposed on the reusable solid propellant rocket engine of the s...
A technical analysis of the solid propellant rocket engines for use with the space shuttle is presen...
The Shuttle flight system is composed of the Orbiter, an External Tank (ET) that contains the ascent...
An analysis of the solid propellant rocket engines for use with the space shuttle booster was conduc...
The launch of the Space Shuttle creates two large exhaust plumes. They are commonly called the groun...
As part of the Shuttle Exhaust Effects Panel (SEEP) program for fiscal year 1973, a limited study wa...
The factors affecting the choice of the 156 inch diameter, parallel burn, solid propellant rocket en...
A systems requirements analysis for the solid propellant rocket engine to be used with the space shu...
The technical requirements for the solid propellant rocket engine to be used with the space shuttle ...
An analysis and design effort was conducted as part of the study of solid rocket motor for a space s...
Three independent studies have been conducted for assessing the impact of rocket launches on the ear...
The specifications for the performance, design, development, and test requirements of the P2-156, S3...
Flexseal assemblies, TVC actuators, hydraulic supply system, TVC electronic control unit, flight ins...
This study was undertaken to determine the feasibility of conducting environmental chamber tests on ...
The potential environmental effects of the exhaust products of conventional rocket propellants have ...
An analysis of the water entry loads imposed on the reusable solid propellant rocket engine of the s...
A technical analysis of the solid propellant rocket engines for use with the space shuttle is presen...
The Shuttle flight system is composed of the Orbiter, an External Tank (ET) that contains the ascent...
An analysis of the solid propellant rocket engines for use with the space shuttle booster was conduc...
The launch of the Space Shuttle creates two large exhaust plumes. They are commonly called the groun...
As part of the Shuttle Exhaust Effects Panel (SEEP) program for fiscal year 1973, a limited study wa...
The factors affecting the choice of the 156 inch diameter, parallel burn, solid propellant rocket en...
A systems requirements analysis for the solid propellant rocket engine to be used with the space shu...
The technical requirements for the solid propellant rocket engine to be used with the space shuttle ...
An analysis and design effort was conducted as part of the study of solid rocket motor for a space s...
Three independent studies have been conducted for assessing the impact of rocket launches on the ear...
The specifications for the performance, design, development, and test requirements of the P2-156, S3...
Flexseal assemblies, TVC actuators, hydraulic supply system, TVC electronic control unit, flight ins...
This study was undertaken to determine the feasibility of conducting environmental chamber tests on ...
The potential environmental effects of the exhaust products of conventional rocket propellants have ...
An analysis of the water entry loads imposed on the reusable solid propellant rocket engine of the s...
A technical analysis of the solid propellant rocket engines for use with the space shuttle is presen...
The Shuttle flight system is composed of the Orbiter, an External Tank (ET) that contains the ascent...