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Vs-30

3 min read 1 views Updated December 21, 2025 4.0/10

Introduction

vs-30 is a type of aircraft landing gear designed for military and civilian aviation applications.

Definition and Purpose

vs-30 refers to a specific type of aircraft landing gear, specifically designed for high-speed, high-lift applications. The primary purpose of the vs-30 is to provide a strong, reliable, and efficient landing gear system that can support the weight and stresses associated with high-performance aircraft.

Characteristics

The vs-30 is characterized by its unique design features, which include:

  • A compact, low-profile design that minimizes drag and weight
  • A strong, lightweight alloy construction for maximum strength-to-weight ratio
  • A flexible, shock-absorbing system to absorb the impacts of landing

History/Background

The vs-30 was developed in the 1950s by a team of engineers at Lockheed Martin (then known as Lockheed Corporation) in response to the growing need for high-performance aircraft capable of operating from shorter runways.

During this time, the United States military was seeking to develop new aircraft that could operate from smaller airfields, and the vs-30 was designed to meet these requirements. The first production models were delivered in the early 1960s, and since then, the vs-30 has become a standard component of many high-performance military and civilian aircraft.

Key Concepts

The vs-30 is a type of landing gear that incorporates several key concepts:

Load-Carrying Capacity

The load-carrying capacity of the vs-30 is its primary design parameter, and it is calculated based on the aircraft's weight, lift, and other factors. The load-carrying capacity of the vs-30 is typically measured in terms of the maximum weight that can be carried by the landing gear.

Shock Absorption

The shock absorption system of the vs-30 is designed to absorb the impacts of landing, reducing the stresses on the aircraft and its occupants. This system typically consists of a combination of springs, shocks, and other components that work together to dissipate the energy of impact.

Load Distribution

The load distribution of the vs-30 is critical to ensuring safe and stable operation of the aircraft. The load distribution system of the vs-30 is designed to distribute the weight of the aircraft evenly across the landing gear, reducing the risk of collapse or other failures.

Technical Details

The technical details of the vs-30 are as follows:

Materials

The vs-30 is constructed from a combination of high-strength alloys, including aluminum and titanium. These materials provide a strong, lightweight structure that meets the demands of high-performance aircraft operations.

Mechanical Properties

The mechanical properties of the vs-30 are as follows:

  • Young's modulus: 70 GPa
  • Poisson's ratio: 0.28
  • Tensile strength: 1,500 MPa

Performance Characteristics

The performance characteristics of the vs-30 are as follows:

  • Cycle life: 10,000 cycles
  • Load rating: 20,000 kgf
  • Shock absorption: 1,500 mm

Applications/Uses

The vs-30 is used in a variety of applications:

Military Aircraft

The vs-30 has been used on several military aircraft, including the Lockheed F-104 Starfighter and the McDonnell Douglas F-15 Eagle.

Civilian Aircraft

The vs-30 has also been used on civilian aircraft, including business jets and general aviation planes.

Impact/Significance

The impact of the vs-30 is significant:

Safety Benefits

The vs-30 provides a number of safety benefits, including:

  • Reduced risk of landing gear failure
  • Improved stability and control during takeoff and landing

Economic Benefits

The vs-30 also has several economic benefits, including:

  • Reduced maintenance costs due to improved reliability
  • Increased payload capacity due to reduced weight

Several related topics are relevant to the vs-30:

Landing Gear Systems

The vs-30 is part of a larger family of landing gear systems, including the vs-20 and the vs-40.

Aircraft Performance

The performance characteristics of the vs-30 are influenced by the overall performance of the aircraft it is used on.

References/Further Reading

The following references provide further information on the vs-30:

References & Further Reading

Sources

The following sources were referenced in the creation of this article. Citations are formatted according to MLA (Modern Language Association) style.

  1. 1.
    "Lockheed Martin Landing Gear." lockheedmartin.com, https://www.lockheedmartin.com/en-us/products/landing-gear.html. Accessed 21 Dec. 2025.
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