Add to ORKGA wind-tunnel investigation was performed to determine the aerodynamic characteristics of a proposed lifting-body personnel launch system (PLS) configuration over a Mach range of 0.05 to 20.3. The test configuration had a low-aspect-ratio body with a flat undersurface and three fins on the upper aft body. Data are presented with a minimum of analysis. All of the experimental data were placed in a structured data base using the R:BASE system and are included on a CD-ROM available with this report
Wind tunnel study of aerodynamic characteristics of three scale model multistage launch vehicles at ...
The Advanced Manned Launch System is a proposed near-term technology, two-stage, fully reusable laun...
This paper examines flight-measured subsonic lift and drag characteristics of seven lifting-body and...
A wind-tunnel investigation was performed to determine the aerodynamic characteristics of a proposed...
An investigation was conducted in the Langley Unitary Plan Wind Tunnel at Mach numbers from 1.6 to 4...
The HL-20 is proposed as a possible future manned spacecraft. The configuration consists of a low-as...
An experimental investigation of the static aerodynamic characteristics of a model of one design con...
Wind tunnel tests were made with a scale model of the HL-20 in the Langley Unitary Plan Wind Tunnel....
A 1.75% scale force and moment model of the Space Launch System was tested in the NASA Langley Resea...
Large scale wind tunnel investigation of lifting body with inflatable and rigid afterbod
The investigation was conducted in the Calspan 8-Ft Transonic wind tunnel at Mach numbers from 0.6 t...
Results from analytical and experimental studies of the aerodynamic characteristics of a turbojet-bo...
NASA is currently studying a personnel launch system (PLS) approach to help satisfy the crew rotatio...
A proposed wing body reusable launch vehicle was tested in the Marshall Space Flight Center (MSFC) 1...
To ensure manned access to space, the Personnel Launch System (PLS) is under consideration by NASA a...
Wind tunnel study of aerodynamic characteristics of three scale model multistage launch vehicles at ...
The Advanced Manned Launch System is a proposed near-term technology, two-stage, fully reusable laun...
This paper examines flight-measured subsonic lift and drag characteristics of seven lifting-body and...
A wind-tunnel investigation was performed to determine the aerodynamic characteristics of a proposed...
An investigation was conducted in the Langley Unitary Plan Wind Tunnel at Mach numbers from 1.6 to 4...
The HL-20 is proposed as a possible future manned spacecraft. The configuration consists of a low-as...
An experimental investigation of the static aerodynamic characteristics of a model of one design con...
Wind tunnel tests were made with a scale model of the HL-20 in the Langley Unitary Plan Wind Tunnel....
A 1.75% scale force and moment model of the Space Launch System was tested in the NASA Langley Resea...
Large scale wind tunnel investigation of lifting body with inflatable and rigid afterbod
The investigation was conducted in the Calspan 8-Ft Transonic wind tunnel at Mach numbers from 0.6 t...
Results from analytical and experimental studies of the aerodynamic characteristics of a turbojet-bo...
NASA is currently studying a personnel launch system (PLS) approach to help satisfy the crew rotatio...
A proposed wing body reusable launch vehicle was tested in the Marshall Space Flight Center (MSFC) 1...
To ensure manned access to space, the Personnel Launch System (PLS) is under consideration by NASA a...
Wind tunnel study of aerodynamic characteristics of three scale model multistage launch vehicles at ...
The Advanced Manned Launch System is a proposed near-term technology, two-stage, fully reusable laun...
This paper examines flight-measured subsonic lift and drag characteristics of seven lifting-body and...