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A kind of inflatable jet take-off gliding recovery Martian vehicle and its use method

An aircraft and Mars technology, applied in the field of Mars aircraft, can solve problems such as overweight, insufficient thrust, complex power system structure, etc., and achieve the effects of prolonging the service life, increasing the number of missions, and widening the land area

Active Publication Date: 2021-06-01
BEIHANG UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0006] In view of this, the present invention provides an inflatable jet take-off and gliding recovery Mars aircraft and its use method, which are used to solve the problem of insufficient thrust of traditional aircraft in the Martian atmospheric environment and at the same time solve the problem of complex structure and heavy weight of the power system. To provide a reusable, energy-dense and lighter aircraft

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  • A kind of inflatable jet take-off gliding recovery Martian vehicle and its use method
  • A kind of inflatable jet take-off gliding recovery Martian vehicle and its use method
  • A kind of inflatable jet take-off gliding recovery Martian vehicle and its use method

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Embodiment Construction

[0042] The technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present application. Obviously, the described embodiments are only examples and not intended to limit the present application.

[0043] The embodiment of the present invention provides a kind of inflatable jet take-off gliding recovery Mars aircraft, such as Figure 1-Figure 6 as shown, figure 1 and Figure 4 For the front view of the Mars spacecraft, figure 2 and Figure 5 For the side view of the Mars spacecraft, image 3 and Figure 6 It is a top view of the Mars spacecraft, including: a fuselage 1, a wing 2 connected to the top of the fuselage 1, and an empennage 3 connected to the tail of the fuselage 1; as Figure 7 as shown, Figure 7 It is a cross-sectional view of the fuselage 1, which also includes: an inflatable jet part 4 located inside the fuselage 1; wherein,

[...

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Abstract

The invention discloses an inflatable jet take-off and gliding recovery Mars aircraft and its use method. The compressed gas is used as the power, which can save the aircraft from complex rotating mechanisms, realize the characteristics of light structure, and solve the problem that the lift force is limited by the thin atmosphere of Mars. It is difficult to meet the requirements of staying in the air; moreover, the compressed gas has high energy density and propulsion power, which can not only provide enough thrust for the aircraft in the Martian environment with a thin atmosphere, but also overcome the insufficient thrust of traditional propellers in the Martian atmosphere. It can also drive the aircraft to obtain a higher flight altitude for gliding flight, prolonging the cruising time of the aircraft; in addition, the compressed gas is taken from the atmosphere of Mars and does not need to be carried in advance, which can realize the repeated process of inflating and jetting cycles. The one-time gliding and landing aircraft can increase the number of missions of the aircraft, prolong the service life of the aircraft, and detect a wider range of land.

Description

technical field [0001] The invention relates to the technical field of aircraft aerodynamic layout design, in particular to a Martian aircraft for take-off, gliding and recovery with an inflated jet and a method for using the same. Background technique [0002] Compared with traditional satellites or ground patrols, the Mars spacecraft has the advantages of large measurement range and strong maneuverability. The United States, Europe, Japan and other countries have proposed many designs of Martian aircraft, such as the "Prandtl-m" aircraft and "Mars Helicopter" aircraft of NASA in the United States, and the "Sample Martian Aircraft" aircraft of JAXA in Japan. [0003] Due to the extremely thin atmosphere of Mars, its surface atmospheric density is only equivalent to that of the earth at a height of 27km. This thin atmospheric environment brings great challenges to the design of aircraft. The low atmospheric density and the low Reynolds number effect caused by the low densit...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/10B64G1/40
CPCB64G1/105B64G1/40B64G1/1071
Inventor 蒋崇文李志豪许晨豪高振勋李椿萱
Owner BEIHANG UNIV
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