For the pressure fed engines, detailed trade studies were conducted defining engine features such as thrust vector control methods, thrust chamber construction, etc. This was followed by engine design layouts and booster propulsion configuration layouts. For the pump fed engines parametric performance and weight data was generated for both O2/H2 and O2/RP-1 engines. Subsequent studies resulted in the selection of both LOX/RP-1 and O2/H2 propellants for the pump fed engines. More detailed analysis of the selected LOX/RP-1 and O2/H2 engines was conducted during the final phase of the study
By simply combining two baseline pump-fed LOX/RP-1 Liquid Rocket Boosters (LRBs) with the Denver cor...
The baseline SRM design for the space shuttle employs proven technology based on actual motor firing...
Preliminary identification and evaluation of promising LO2/Hydrocarbon rocket engine cycles were use...
The analyses performed in assessing the merit of the Liquid Rocket Booster concept for use in altern...
Three tasks were undertaken by Eagle Engineering as a part of the Liquid Rocket Booster (LRB) study....
During the past three decades, an enormous amount of resources were expended in the design and devel...
The recommended Liquid Rocket Booster (LRB) concept is shown which uses a common main engine with th...
Preliminary engineering definition information is presented for a liquid pressure-fed reusable boost...
A list is presented of the trade studies which were planned and the status to which they have been a...
Preliminary identification and evaluation of promising liquid oxygen/ hydrocarbon (LO2/HC) rocket en...
The engine weight, mass properties data, and engine design criteria and specifications are presented...
This study identifies and evaluates promising LO2/HC rocket engine cycles, produces a consistent and...
A study was conducted to analyze the characteristics and performance data for the booster vehicles t...
The impacts of introducing liquid rocket booster engines (LRB) into the Space Transportation System ...
An advanced LOX/LH2 engine study for the use of NASA and vehicle prime contractors in developing con...
By simply combining two baseline pump-fed LOX/RP-1 Liquid Rocket Boosters (LRBs) with the Denver cor...
The baseline SRM design for the space shuttle employs proven technology based on actual motor firing...
Preliminary identification and evaluation of promising LO2/Hydrocarbon rocket engine cycles were use...
The analyses performed in assessing the merit of the Liquid Rocket Booster concept for use in altern...
Three tasks were undertaken by Eagle Engineering as a part of the Liquid Rocket Booster (LRB) study....
During the past three decades, an enormous amount of resources were expended in the design and devel...
The recommended Liquid Rocket Booster (LRB) concept is shown which uses a common main engine with th...
Preliminary engineering definition information is presented for a liquid pressure-fed reusable boost...
A list is presented of the trade studies which were planned and the status to which they have been a...
Preliminary identification and evaluation of promising liquid oxygen/ hydrocarbon (LO2/HC) rocket en...
The engine weight, mass properties data, and engine design criteria and specifications are presented...
This study identifies and evaluates promising LO2/HC rocket engine cycles, produces a consistent and...
A study was conducted to analyze the characteristics and performance data for the booster vehicles t...
The impacts of introducing liquid rocket booster engines (LRB) into the Space Transportation System ...
An advanced LOX/LH2 engine study for the use of NASA and vehicle prime contractors in developing con...
By simply combining two baseline pump-fed LOX/RP-1 Liquid Rocket Boosters (LRBs) with the Denver cor...
The baseline SRM design for the space shuttle employs proven technology based on actual motor firing...
Preliminary identification and evaluation of promising LO2/Hydrocarbon rocket engine cycles were use...