• Nenhum resultado encontrado

J. Aerosp. Technol. Manag. vol.8 número2

N/A
N/A
Protected

Academic year: 2018

Share "J. Aerosp. Technol. Manag. vol.8 número2"

Copied!
1
0
0

Texto

(1)

J. Aerosp. Technol. Manag., São José dos Campos, Vol.8, No 2, pp.121-121, Apr.-Jun., 2016

Systems Engineering

William W. Vaughan1

T

he term “systems engineering”, when entered into the Google search page, produces a signiicant number of results, evidence that systems engineering is recognized as being important for the success of essentially all products. Since most readers of this item will be rather well versed in documents concerning systems engineering, I have elected to share some of the points made on this subject in a document developed by the European Cooperation for Space Standardization (ECSS), a component of the European Space Agency (Anon 2009).

he ECSS document deines systems engineering as “an interdisciplinary approach governing the total technical efort to transform requirements into a system solution”. hese requirements include hardware, sotware, irmware, human resources, information, techniques, facilities, services, and other support elements. he systems engineering process is intrinsically iterative across the whole life cycle of the project and is produced under the leadership of engineering talents with technical excellence attributes. Systems engineering is not an administrative focused or led function. Technical excellence is the key to successful systems engineering and, thus, to a successful project.

An article that addressed new synergies between systems engineering and diminishment of manufacturing sources and material shortages made two important points (Bracuto et al. 2010):

doi: 10.5028/jatm.v8i2.634

1.NASA Emeritus –NASA Marshall Space Flight Center – Huntsville/AL – USA.

Author for correspondence:William W. Vaughan | NASA Marshall Space Flight Center | 4200 Rideout Rd | Huntsville, AL 35808 – USA | Email: [email protected]

Anon (2009) European Cooperation for Space Standardization. System Engineering General Requirements. ECSS-E-ST-10C, March 6, 2009.

Bracuto C, Melnikow A, Zelinski E (2010) New synergies between systems engineering and DMSMS. Defense Standardization Program Journal, January/March 2010, pp 3-10.

Dannenberg KK (1974) Management philosophies as applied to major NASA programs. NASA-CR-141258. Washington, DC: National Aeronautics and Space Administration.

REFERENCES

NOTE: his editorial is based on “Technical Excellence: A Requirement for Good

Engineering” (AIAA-2008-1120), prepared and presented by the author at the 47th

American Institute of Aeronautics and Astronautics Aerospace Sciences Meeting,

January 7-11, 2008, Reno, NV, USA.

Referências

Documentos relacionados

he evaluation of antioxidant performance during thermal ageing was achieved by submitting withdrawn samples to sol/gel extraction, swelling and mechanical testing, dynamical

he composition is less sensitive than RDX in sensitivity tests, it has good stability proprieties and is compatible with the DOPE lacquer used to assemble and seal

ABSTRACT: The design, prototyping, and free-space measurement of a 6-GHz Frequency Selective Surface ilter is presented.. The prototyping resolution of a large (A4 sheet

his paper presented an evaluation of the diference in the IMMPDAF algorithm performance using real and simulated measurements for the same target trajectory. hese radar

slip-type strong scattering source on the Inverse Synthetic Aperture Radar (ISAR) imaging plane under the three forms of micro-motion of nutation, precession and spinning is

he present investigation intends to report some experiences for computing aeroelastic damping trends as a function of light speed, based on an output-only modal parameter extraction

he present study resulted in four individual cognitive maps and a congregated map that allowed identifying the diiculties in requirements elicitation process for building

In this study, an aerodynamic airfoil shape design has been conducted to increase the maximum lit coeicient and the maximum lit-to-drag ratio using the Adaptive Range Multi-