Some of the environments and loads experienced by the Space Shuttle or future reusable space vehicles are unique, while others are similar to those encountered by commercial and/or military aircraft. Prior to the Space Transportation System (STS) flights, fatigue loads spectra were generated for the Space Shuttle based on anticipated environments and assumptions that were shown not to be applicable to the actual flight environments the vehicle experienced. This resulted in the need to generate a new cycle of fatigue loads spectra, which was based on measured flight data as well as mission profiles, reflecting the various types of service and operations the vehicle and payloads experienced
The model reference control of lumped linear systems and the model reference control of the distribu...
The variability in initial crack size and fatigue crack growth is incorporated in a probabilistic mo...
Small Satellite Technology Initiative (SSTI) Lewis Spacecraft Program is evaluated. Spacecraft integ...
A methodology for simulating the growth of long through cracks in the skin of pressurized aircraft f...
Future satellite communications is expected to be fully integrated into National and Global Informat...
The main objectives are: a model of a replicated system with exact-match voting; a fault model that ...
The Space Transportation System (STS) documents were reviewed to determine their applicability to th...
A study was conducted to evaluate ultrasonic cleaning systems for precision cleaning effectiveness f...
Volume two of the facilities catalogue deals with Airbreathing Propulsion and Flight Simulation Faci...
Turbo coding using iterative SOVA decoding and M-ary differentially coherent or non-coherent modulat...
Boeing's view of the High Speed Civil Transport (HSCT) is given in viewgraph format. Boeing believes...
This report covers a portion of an ongoing investigation of the durability of titanium alloys for th...
The TRMM (Tropical Rain Measuring Mission) Study shows the feasibility of a conically scanned, total...
To assist analysis of riveted lap joints, stress intensity factors are determined for surface and co...
NASA-Langley is sponsoring a rotorcraft structural dynamics program with the objective to establish ...
The model reference control of lumped linear systems and the model reference control of the distribu...
The variability in initial crack size and fatigue crack growth is incorporated in a probabilistic mo...
Small Satellite Technology Initiative (SSTI) Lewis Spacecraft Program is evaluated. Spacecraft integ...
A methodology for simulating the growth of long through cracks in the skin of pressurized aircraft f...
Future satellite communications is expected to be fully integrated into National and Global Informat...
The main objectives are: a model of a replicated system with exact-match voting; a fault model that ...
The Space Transportation System (STS) documents were reviewed to determine their applicability to th...
A study was conducted to evaluate ultrasonic cleaning systems for precision cleaning effectiveness f...
Volume two of the facilities catalogue deals with Airbreathing Propulsion and Flight Simulation Faci...
Turbo coding using iterative SOVA decoding and M-ary differentially coherent or non-coherent modulat...
Boeing's view of the High Speed Civil Transport (HSCT) is given in viewgraph format. Boeing believes...
This report covers a portion of an ongoing investigation of the durability of titanium alloys for th...
The TRMM (Tropical Rain Measuring Mission) Study shows the feasibility of a conically scanned, total...
To assist analysis of riveted lap joints, stress intensity factors are determined for surface and co...
NASA-Langley is sponsoring a rotorcraft structural dynamics program with the objective to establish ...
The model reference control of lumped linear systems and the model reference control of the distribu...
The variability in initial crack size and fatigue crack growth is incorporated in a probabilistic mo...
Small Satellite Technology Initiative (SSTI) Lewis Spacecraft Program is evaluated. Spacecraft integ...