An orbital maneuvering vehicle (OMV) front end kit is defined which is capable of performing in-situ fluid resupply and modular maintenance of free flying spacecraft based on the integrated orbital servicing system (IOSS) concept. The compatibility of the IOSS to perform gas and fluid umbilical connect and disconnect functions utilizing connect systems currently available or in development is addressed. A series of tasks involving on-orbit servicing and the engineering test unit (ETU) of the on-orbit service were studied. The objective is the advancement of orbital servicing by expanding the Spacecraft Servicing Demonstration Plan (SSDP) to include detail demonstration planning using the Multimission Modular Spacecraft (MMS) and upgrading t...
A general purpose FORTRAN program for simulating and optimizing point mass trajectories (POST) of ae...
The lunar construction utility vehicle (LCUV) is an all-purpose construction vehicle which will aid ...
The level C software formulations requirements for the entry guidance and the simplified autopilot t...
The objective of this program is to develop generic load models with multiple levels of progressive ...
A design and analysis study was conducted to provide advanced engine descriptions and parametric dat...
The overall purpose of the Electrolysis Performance Improvement Concept Study flight experiment is t...
Technical and management studies defining Apollo applications program payload integration task
The Space Shuttle Redesigned Solid Rocket Motor (RSRM) Certification Program provides confidence tha...
The first assessment is made of the design requirements and conceptual definition of a front end kit...
A functional description of the ATAMM Multicomputer Operating System is presented. ATAMM (Algorithm ...
This document is the final report for the Clearfield disassembly evaluation and a continuation of th...
Multicomputer configurations and redundancy management techniques used in various airborne systems w...
The scope of the study is to investigate ways of controlling the microgravity environment of the Int...
The Advanced Cockpit Controls/Advanced Flight Control System (ACC/AFCS) study was conducted by the B...
The EDIN (Engineering Design Integration) System which provides a collection of hardware and softwar...
A general purpose FORTRAN program for simulating and optimizing point mass trajectories (POST) of ae...
The lunar construction utility vehicle (LCUV) is an all-purpose construction vehicle which will aid ...
The level C software formulations requirements for the entry guidance and the simplified autopilot t...
The objective of this program is to develop generic load models with multiple levels of progressive ...
A design and analysis study was conducted to provide advanced engine descriptions and parametric dat...
The overall purpose of the Electrolysis Performance Improvement Concept Study flight experiment is t...
Technical and management studies defining Apollo applications program payload integration task
The Space Shuttle Redesigned Solid Rocket Motor (RSRM) Certification Program provides confidence tha...
The first assessment is made of the design requirements and conceptual definition of a front end kit...
A functional description of the ATAMM Multicomputer Operating System is presented. ATAMM (Algorithm ...
This document is the final report for the Clearfield disassembly evaluation and a continuation of th...
Multicomputer configurations and redundancy management techniques used in various airborne systems w...
The scope of the study is to investigate ways of controlling the microgravity environment of the Int...
The Advanced Cockpit Controls/Advanced Flight Control System (ACC/AFCS) study was conducted by the B...
The EDIN (Engineering Design Integration) System which provides a collection of hardware and softwar...
A general purpose FORTRAN program for simulating and optimizing point mass trajectories (POST) of ae...
The lunar construction utility vehicle (LCUV) is an all-purpose construction vehicle which will aid ...
The level C software formulations requirements for the entry guidance and the simplified autopilot t...