Add to ORKGThe utilization of the Shuttle-C Heavy Lift Launch Vehicle (HLLV) to augment the Shuttle orbiter to deliver to earth orbit elements for assembly of a rephased definition of Space Station Freedom is assessed. A past history of previous HLLV studies performed with respect to Freedom launch and assembly is reviewed and conclusions extrapolated that are appropriate to consider for the new rephased Freedom definition. The rephased Freedom definition is explained, two utilization scenarios are developed and related assessments are provided for Shuttle-C utilization early in the assembly sequence or utilization later in theon-orbit build up phase
Volume two of the facilities catalogue deals with Airbreathing Propulsion and Flight Simulation Faci...
Loads analysis for structural dynamic systems is usually performed by finite element models. Because...
Equations of motion, control strategy, perturbation, rigid-body maneuvers, quasi-modal equations, an...
A ground vibration test was performed on the AH-64 (Apache) helicopter to determine the frequency re...
A 203rd order simulation model was developed to evaluate the space station customer accommodation pa...
Analysis and design methods for laminated composite materials have been the subject of considerable ...
A listing is given of those satellites currently in orbit and those that have previously orbited the...
Orbit Transfer Vehicle (OTV) processing at the space station is divided into two major categories: O...
The Construction of Facilities (CoF) appropriation provides contractual services for the repair, reh...
Information on the Tethered Gravity Laboratory on the International Space Station is given in viewgr...
The Timed Doppler Interferometer (TIDI) will accurately and precisely determine the global vector ML...
The purpose is to summarize a Phase 1 SBIR project performed for the NASA/Langley Computational Stru...
The results of tests to assess capacity loss in nickel hydrogen cells are presented in outline form....
A brief summary is given of the key objectives of Task 5 of the Space Station Accommodations Concept...
The issue of technology advancement and future space transportation vehicles is addressed. The chall...
Volume two of the facilities catalogue deals with Airbreathing Propulsion and Flight Simulation Faci...
Loads analysis for structural dynamic systems is usually performed by finite element models. Because...
Equations of motion, control strategy, perturbation, rigid-body maneuvers, quasi-modal equations, an...
A ground vibration test was performed on the AH-64 (Apache) helicopter to determine the frequency re...
A 203rd order simulation model was developed to evaluate the space station customer accommodation pa...
Analysis and design methods for laminated composite materials have been the subject of considerable ...
A listing is given of those satellites currently in orbit and those that have previously orbited the...
Orbit Transfer Vehicle (OTV) processing at the space station is divided into two major categories: O...
The Construction of Facilities (CoF) appropriation provides contractual services for the repair, reh...
Information on the Tethered Gravity Laboratory on the International Space Station is given in viewgr...
The Timed Doppler Interferometer (TIDI) will accurately and precisely determine the global vector ML...
The purpose is to summarize a Phase 1 SBIR project performed for the NASA/Langley Computational Stru...
The results of tests to assess capacity loss in nickel hydrogen cells are presented in outline form....
A brief summary is given of the key objectives of Task 5 of the Space Station Accommodations Concept...
The issue of technology advancement and future space transportation vehicles is addressed. The chall...
Volume two of the facilities catalogue deals with Airbreathing Propulsion and Flight Simulation Faci...
Loads analysis for structural dynamic systems is usually performed by finite element models. Because...
Equations of motion, control strategy, perturbation, rigid-body maneuvers, quasi-modal equations, an...