Add to ORKGThe technical effort associated with the selection and definition of the recommended SRB-X concept is documented. Included are discussions concerning the trades leading to the selected concept, the analysis that established the concept's basic subsystem characteristics, selected configuration description and performance capabilities, launch site operations and facility needs, development schedule, cost characteristics, risk assessment, and a cursory comparison with other launch systems
The topics covered include the following: (1) the next manned space transportation system; (2) devel...
This paper describes future space transportation launch vehicles presently under study by the NASA a...
A study was conducted in a trisonic wind tunnel to determine the load distribution over the external...
A technical analysis of the solid propellant rocket engines for use with the space shuttle is presen...
A study for the selection of a low cost shuttle system for design and development was conducted. The...
The technical requirements for the solid propellant rocket engine to be used with the space shuttle ...
Additional technical data have been prepared to supplement the data supplied in the SRM shuttle boos...
The purpose of this study was to determine the feasibility of Liquid Rocket Boosters (LRBs) replacin...
The solid rocket boosters assembly environment is described in terms of the contraints it places upo...
The Phase B Extension of the Space Shuttle System Program Definition study was redirected to apply p...
A study was conducted to analyze the characteristics and performance data for the booster vehicles t...
The design of the spacecraft is described. Focus is placed on the external tanks, the solid rocket b...
An analysis of the solid propellant rocket engines for use with the space shuttle booster was conduc...
Historical weight estimating relationships were developed for the liquid rocket booster (LRB) using ...
The baseline SRM design for the space shuttle employs proven technology based on actual motor firing...
The topics covered include the following: (1) the next manned space transportation system; (2) devel...
This paper describes future space transportation launch vehicles presently under study by the NASA a...
A study was conducted in a trisonic wind tunnel to determine the load distribution over the external...
A technical analysis of the solid propellant rocket engines for use with the space shuttle is presen...
A study for the selection of a low cost shuttle system for design and development was conducted. The...
The technical requirements for the solid propellant rocket engine to be used with the space shuttle ...
Additional technical data have been prepared to supplement the data supplied in the SRM shuttle boos...
The purpose of this study was to determine the feasibility of Liquid Rocket Boosters (LRBs) replacin...
The solid rocket boosters assembly environment is described in terms of the contraints it places upo...
The Phase B Extension of the Space Shuttle System Program Definition study was redirected to apply p...
A study was conducted to analyze the characteristics and performance data for the booster vehicles t...
The design of the spacecraft is described. Focus is placed on the external tanks, the solid rocket b...
An analysis of the solid propellant rocket engines for use with the space shuttle booster was conduc...
Historical weight estimating relationships were developed for the liquid rocket booster (LRB) using ...
The baseline SRM design for the space shuttle employs proven technology based on actual motor firing...
The topics covered include the following: (1) the next manned space transportation system; (2) devel...
This paper describes future space transportation launch vehicles presently under study by the NASA a...
A study was conducted in a trisonic wind tunnel to determine the load distribution over the external...