• Nenhum resultado encontrado

J. Aerosp. Technol. Manag. vol.6 número1

N/A
N/A
Protected

Academic year: 2018

Share "J. Aerosp. Technol. Manag. vol.6 número1"

Copied!
9
0
0

Texto

Loading

Imagem

Table 1. Airship design requirements.
Figure 1. Scheme for determination of baseline specii cations of an airship.
Table 4. Speciications of the engine.
Table 5. Component mass and center of gravity distribution.
+4

Referências

Documentos relacionados

In order to manage the dificulties to model the software behavior the approach employs the Conformance and Fault Injection (CoFI) testing methodology associated with the

With that in mind, this research paper analyzed the applicability and relevance of open innovation within a diferent product development context in the Brazilian aerospace

Besides, the development models on thrust chamber, turbopump and gas generator (power pack), valves and regulators and control system level, two DM, one EM and two QM on engine

Since its founding, the ABEC Brasil has always had as a goal to ensure publishing standards of form and content of technical and scientiic publications in the country; to keep

2: the Irradiator Module, with four slots, loaded with biological material that is irradiated during the DRM experiment; the Fan Module, responsible for maintaining the

Finally, we highlight some capabilities and limitations inherent in the technology of lasers and present some applications in defense and attack operations enabled by

Looking back in time, the JAESA was created in 2007 as a technical journal, objective of which was publishing papers of research and development in aerospace engineering and

What is presented within this paper is a discussion of (1) atmospheric density versus altitude, (2) the atmospheric thermodynamic parameters and how they were applied within the