The Liquid Rocket Booster study was initiated by NASA to define an alternative to the Solid Rocket Boosters used on the STS. These studies have involved MSFC, JSC and KSC and their contractors. The prime study contractors, Martin Marietta Corporation and General Dynamics Space Systems, have identified Liquid Booster configurations which would replace the SRB\u27s in the Shuttle stack. The Liquid Rocket Booster increases Shuttle performance to 70K LBS, provides improved reliability, hold down and verification prior to vehicle release, engine out and improved abort capability, and is phased into the STS launch operations without adversely affecting flight rate
The projected 24000 pound payload lift capability for the baseline Space Shuttle, with anticipated a...
The technical requirements for the solid propellant rocket engine to be used with the space shuttle ...
The impacts of introducing liquid rocket booster engines (LRB) into the Space Transportation System ...
The impacts of introducing Liquid Rocket Boosters (LRB) into the STS/KSC launch environment are iden...
The factors affecting the choice of the 156 inch diameter, parallel burn, solid propellant rocket en...
The cancellation of the Advanced Solid Rocket Booster Project and the earth-to-orbit payload require...
This paper surveys the basic configuration options available to a Liquid Fly Back Booster (LFBB), in...
An operation and schedule enhancement is shown that replaces the four-body cluster (Space Shuttle Or...
Three tasks were undertaken by Eagle Engineering as a part of the Liquid Rocket Booster (LRB) study....
Two Solid Rocket Boosters provide the primary first stage thrust for the Space Shuttle. These Booste...
The paper will cover the current status of three major propulsion elements for the Space Transportat...
The National Aeronautics and Space Administration's (NASA's) Space Launch System (SLS) Program, mana...
The impacts of introducing liquid rocket booster engines (LRB) into the Space Transportation System ...
The impacts of introducing liquid rocket booster engines (LRB) into the Space Transportation System ...
An analysis and design effort was conducted as part of the study of solid rocket motor for a space s...
The projected 24000 pound payload lift capability for the baseline Space Shuttle, with anticipated a...
The technical requirements for the solid propellant rocket engine to be used with the space shuttle ...
The impacts of introducing liquid rocket booster engines (LRB) into the Space Transportation System ...
The impacts of introducing Liquid Rocket Boosters (LRB) into the STS/KSC launch environment are iden...
The factors affecting the choice of the 156 inch diameter, parallel burn, solid propellant rocket en...
The cancellation of the Advanced Solid Rocket Booster Project and the earth-to-orbit payload require...
This paper surveys the basic configuration options available to a Liquid Fly Back Booster (LFBB), in...
An operation and schedule enhancement is shown that replaces the four-body cluster (Space Shuttle Or...
Three tasks were undertaken by Eagle Engineering as a part of the Liquid Rocket Booster (LRB) study....
Two Solid Rocket Boosters provide the primary first stage thrust for the Space Shuttle. These Booste...
The paper will cover the current status of three major propulsion elements for the Space Transportat...
The National Aeronautics and Space Administration's (NASA's) Space Launch System (SLS) Program, mana...
The impacts of introducing liquid rocket booster engines (LRB) into the Space Transportation System ...
The impacts of introducing liquid rocket booster engines (LRB) into the Space Transportation System ...
An analysis and design effort was conducted as part of the study of solid rocket motor for a space s...
The projected 24000 pound payload lift capability for the baseline Space Shuttle, with anticipated a...
The technical requirements for the solid propellant rocket engine to be used with the space shuttle ...
The impacts of introducing liquid rocket booster engines (LRB) into the Space Transportation System ...