Sacrificial Connector Saver for Rocket Launcher Protection

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Solution Overview

Problem

Existing rocket launchers face challenges in maintaining reliable electrical communication between smart rockets and the launcher due to extreme conditions during launch, leading to potential damage of connectors and increased reloading times in battle scenarios.

Innovation Solution

A guidance section connector interface system that includes a sacrificial connector saver to protect the launcher connector by forming a dominant connection with it during launch, ensuring the connector saver remains attached to the launcher connector, thus shielding it from blast effects and allowing for quick and reliable 'smart' rocket launches.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Extent of automation

If electrical connections are made between smart rockets and launcher for guidance communication, then rocket intelligence and targeting capability is improved, but connector reliability deteriorates due to extreme launch conditions

Engineering Contradiction:
Improverocket intelligenceVSAvoidconnector reliability
Core Design Contradiction:
Extent of automationVSReliability

Solution Approach 1:

The connector system is divided into two separate components: a reusable launcher connector and a disposable connector saver attached to the rocket. This segmentation allows the launcher connector to be protected from extreme launch conditions while the connector saver absorbs the thermal and mechanical stress, enabling reliable guidance communication without compromising connector reliability

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The connector saver is designed as a disposable component that is attached to the rocket and discarded after launch. It serves as a sacrificial element that protects the expensive reusable launcher connector from damage during launch, allowing the launcher connector to remain reliable for multiple uses while the disposable connector saver absorbs the extreme conditions

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

2Reliability

If connector saver remains attached to launcher connector during launch, then launcher connector is protected from blast effects, but device complexity increases

Engineering Contradiction:
Improvelauncher connector protectionVSAvoidconnector interface complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The connector saver is designed to nest over the launcher connector during launch, with the launcher connector positioned inside the connector saver's protective structure. This nested arrangement allows the connector saver to shield the launcher connector from blast effects while maintaining a compact integrated design that does not significantly increase overall device complexity

Inventive Principle:
Principle #7Nested doll (Nesting)

3Productivity

If sacrificial connector saver is used to protect launcher connector, then reloading time is reduced, but manufacturing complexity increases

Engineering Contradiction:
Improvereloading speedVSAvoidconnector manufacturing
Core Design Contradiction:
ProductivityVSEase of manufacture

Solution Approach 1:

The connector saver is merged with the rocket body as an integrated component, combining the rocket structure with the protective connector housing. This merging eliminates the need for separate assembly steps and simplifies manufacturing, allowing the connector saver to be produced as part of the rocket manufacturing process rather than as a separate component requiring additional assembly

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS9163901B2Guidance section connector interface for advanced rocket launchers
Publication Date: 2015.10.20 VERTEX AEROSPACE LLC
  • US9163901B2 patent drawing
  • US9163901B2 patent drawing
  • US9163901B2 patent drawing

AI summary

A guidance section connector interface system operable with smart or guided rockets to be launched from a rocket launcher comprising a rocket connector of a rocket in electronic communication with a guidance system of a guidance head of the rocket, a connector saver, and a launcher connector of a rocket launcher. The connector saver can be configured to connect the rocket connecter to the launcher connector. The connection between the connector saver and the rocket connector is configured to release upon launching the rocket, wherein the connector saver remains connected to the launcher connector to protect the launcher connector from the extreme conditions within the rocket launcher at launch.