scholarly journals Key Terrestrial and Space Environment Sources

Author(s):  
Dale L. Johnson ◽  
William W. Vaughan

Natural (Terrestrial & Space) Environment (NE) phenomena play a significant role in the design and flight of aerospace vehicles and in the integrity of the associated aerospace systems and structures. Both the terrestrial environment (0-90 km altitude) and the space environment (Earth orbital altitudes) parameters and their engineering application philosophy are given with emphasis on launch vehicle-affected terrestrial environment elements. This paper will describe the key terrestrial and space environment sources: wind; atmospheric; and orbital models used in the design and development of launch/space vehicles.

Author(s):  
Dale L. Johnson ◽  
William W. Vaughan

Natural (Terrestrial & Space) Environment (NE) phenomena play a significant role in the design and flight of aerospace vehicles and in the integrity of the associated aerospace systems and structures. Natural environmental design criteria guidelines described here are based on measurements and modeling of atmospheric and climatic phenomena relative to various aerospace vehicle development and mission/operational procedures, and for vehicle launch locations. Both the terrestrial environment (0-90 km altitude) and the space environment (Earth orbital altitudes) parameters and their engineering application philosophy are given with emphasis on launch vehicle-affected terrestrial environment elements. This paper also addresses the basis for the NE guidelines presented, the interpretation of the guidelines, and application to the development of launch or space vehicle design requirements. This paper represents the first of three on this subject.


1997 ◽  
Author(s):  
Steven Pearson ◽  
William Vaughan ◽  
Glen Batts ◽  
Gwenevere Jasper ◽  
Steven Pearson ◽  
...  

2011 ◽  
Vol 92 (9) ◽  
pp. 1149-1157 ◽  
Author(s):  
William W. Vaughan ◽  
Dale L. Johnson

Aerospace meteorology plays an important role in the design, development, and operation of aerospace vehicles. Many of the issues and lessons presented occurred during the involvement of the authors with the development and interpretation of aerospace environment inputs, especially those of the terrestrial environment. Background for the actions needed to avoid the issue being repeated or the lesson having to be relearned is addressed. The engineering application importance and some issues associated with the presentation and interpretation of terrestrial environment guidelines associated with aerospace meteorology elements are presented.


1998 ◽  
Vol 13 (1) ◽  
pp. 25-30 ◽  
Author(s):  
Jianping Yuan ◽  
Huamin Jia ◽  
Qun Fang

Author(s):  
Pedro J. Medelius ◽  
Dave Bartine

For the successful integration of new sensors into space vehicles, it is necessary to establish early in the project a close and interactive between the technology developer and the end user. The problem to be solved and prospective solutions required from the technology developer should be clearly identified and well defined to demonstrate that the proposed technology works satisfactorily in the relevant environment and that it presents no danger or interference to existing systems. The technology provider has to remain involved with the user through installation, acceptance testing, and acclimation of the new technology. The product developer and end user must jointly perform the following functions: • Develop a detailed set of requirements: performance, physical, environmental, safety, reliability, and maintainability. • Establish the qualification process to certify the product. • Define the documentation requirements for the qualification process. • Establish a quality control process to monitor the design, fabrication, testing, and integration of the product into the vehicle or the ground support system. It is important that the performance requirements established by the user be well defined before any potential solution to a problem is considered viable. The successful integration of micro- and nanotechnology into space vehicles requires a coordinated effort throughout the design, development, installation, and integration processes. The selection of materials for sensors and associated instrumentation is critical because certain materials can cause hazards in the space environment that are not apparent in the ground environment. Materials should be selected early, and their use approved by the user. The safety community should be involved early in the design process, even during the conceptual design phase. Certification and safety problems that are often found late in the design cycle can be avoided easily and less expensively if they are addressed early in the process. Flight and ground operations personnel should also contribute to the design process since they are the people who will be installing sensors and instrumentation, as well as operating the systems. They understand the vehicle and support systems that will be required to support the installation and operation of new systems.


1986 ◽  
Vol 30 (4) ◽  
pp. 370-373
Author(s):  
Barry Tillman

Nasa is developing a Man/System Integration Standard. It is to be a single source for human factors engineering standards for the design and development of space habitats. Included in this paper is a discussion of the Anthropometrics, Architecture, Activity Centers, and Health Management sections of the standard. There is a brief description of the general contents of each of these sections and some of the human factors considerations that are unique to the space environment.


2021 ◽  
Vol 9 (1) ◽  
pp. 62-67
Author(s):  
Erika B. Wagner

Abstract Blue Origin's New Shepard launch vehicle made its first flight above the Kármán Line, returning safely to Earth in November 2015. At the time when this paper is being written (February 2021), the system has conducted 14 flights, including 10 with research and education payloads aboard. More than 100 payloads have exercised a wide range of capabilities and interfaces, from small cubesat-form factor student payloads to large custom payloads of nearly 100 kg. Investigations have spanned a wide range of high-altitude and microgravity research objectives, as well as raising technology readiness level (TRL) on diverse hardware. This paper summarizes New Shepard's payload missions to date, and presents standardized and custom accommodations, both in the shirtsleeve cabin and directly exposed to the space environment.


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