The lunar construction utility vehicle (LCUV) is an all-purpose construction vehicle which will aid in the robotic assembly of a lunar outpost. The LCUV will have the following capabilities: (1) must be self supporting including repairs; (2) must offload itself from a lunar lander; (3) must be telerobotic and semi-autonomous; (4) must be able to transport one space station common module; (5) must allow for man-rated operation; and (6) must be able to move lunar regolith for site preparation. This study recommends the use of an elastic tracked vehicle. Detailed material analyses of most of the LCUV components were accomplished. The body frame, made of pinned truss elements, was stress analyzed using NASTRAN. A track connection system was dev...
The Defense Advanced Research Projects Agency (DARPA) inaugurated a program addressing research and ...
This paper presents a description of a model for a space vehicle operational scenario and the comman...
A three-inch mean diameter, two-stage turbine with partial admission in each stage was experimentall...
In order to prepare a site for a manned lunar base, an autonomously operated construction vehicle is...
The LAWS phase 1 and phase 2 studies have been completed on schedule and have led to significant adv...
A set of construction and assembly tasks required on the lunar surface was developed, different conc...
Lockheed personnel, along with team member subcontractors and consultants, have performed a prelimin...
The feasibility of replacing the Space Transportation System (STS) Solid Rocket Boosters (SRBs) with...
The Advanced Cockpit Controls/Advanced Flight Control System (ACC/AFCS) study was conducted by the B...
An investigation was made to determine the feasibility of using an aerobrake system for manned and u...
The EDIN (Engineering Design Integration) System which provides a collection of hardware and softwar...
Many state Departments of Transportation (DOT) across the US, including MnDOT, are experiencing prob...
Volume 1 of the Final Study Report provides an Executive Summary of the Phase B study effort conduct...
Structural design of spacecraft subjected to thermal sterilization prior to planetary landin
A preliminary design of a two-stage to orbit vehicle was conducted with the requirements to carry a ...
The Defense Advanced Research Projects Agency (DARPA) inaugurated a program addressing research and ...
This paper presents a description of a model for a space vehicle operational scenario and the comman...
A three-inch mean diameter, two-stage turbine with partial admission in each stage was experimentall...
In order to prepare a site for a manned lunar base, an autonomously operated construction vehicle is...
The LAWS phase 1 and phase 2 studies have been completed on schedule and have led to significant adv...
A set of construction and assembly tasks required on the lunar surface was developed, different conc...
Lockheed personnel, along with team member subcontractors and consultants, have performed a prelimin...
The feasibility of replacing the Space Transportation System (STS) Solid Rocket Boosters (SRBs) with...
The Advanced Cockpit Controls/Advanced Flight Control System (ACC/AFCS) study was conducted by the B...
An investigation was made to determine the feasibility of using an aerobrake system for manned and u...
The EDIN (Engineering Design Integration) System which provides a collection of hardware and softwar...
Many state Departments of Transportation (DOT) across the US, including MnDOT, are experiencing prob...
Volume 1 of the Final Study Report provides an Executive Summary of the Phase B study effort conduct...
Structural design of spacecraft subjected to thermal sterilization prior to planetary landin
A preliminary design of a two-stage to orbit vehicle was conducted with the requirements to carry a ...
The Defense Advanced Research Projects Agency (DARPA) inaugurated a program addressing research and ...
This paper presents a description of a model for a space vehicle operational scenario and the comman...
A three-inch mean diameter, two-stage turbine with partial admission in each stage was experimentall...