Separable Projectile Payload Container for Test and Effect Conversion

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Solution Overview

Problem

Existing separable projectile designs are inadequate for safely recovering sensitive measuring equipment during testing, as they often result in damage, and lack flexibility for modifying between test and effect embodiments.

Innovation Solution

A method and arrangement for modifying a separable projectile by changing the payload container from measuring equipment to effect parts, using a separation charge, such as a propellant or pyrotechnic primer, to safely separate the payload container from the projectile, allowing for easy conversion between test and effect embodiments, and incorporating a parachute for recovery.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If the projectile is designed as a separable projectile with effect charges, then terminal effect capability is improved, but the projectile cannot be used for testing measuring equipment during acceleration and trajectory phase

Engineering Contradiction:
Improvedual-use capabilityVSAvoidpayload container configuration
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The projectile is divided into separable components: a reusable projectile body and a replaceable payload container. The payload container can be detached and replaced to switch between test embodiment (with measuring equipment) and effect embodiment (with effect charges), enabling dual-use capability without redesigning the entire system.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The projectile body is designed with universal interfaces and attachment mechanisms that can accommodate different types of payload containers. This allows the same projectile body to serve multiple functions by simply changing the payload container, supporting both testing and operational missions.

Inventive Principle:
Principle #6Universality (Multi-functionality)

2Adaptability or versatility

If the projectile is designed for terminal effect only, then terminal effect capability is improved, but it cannot be modified for testing measuring equipment during acceleration and trajectory phase

Engineering Contradiction:
Improveembodiment conversion capabilityVSAvoidmodification process
Core Design Contradiction:
Adaptability or versatilityVSEase of manufacture

Solution Approach 1:

The payload container is designed as a separate, pre-configured module that can be attached to the projectile body without complex assembly. This segmentation allows the container to be manufactured and tested independently, then quickly installed on the projectile body, simplifying the modification process between different embodiments.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The payload containers are pre-configured and pre-tested in their respective embodiments (test or effect) before being attached to the projectile body. This preliminary preparation reduces on-site modification complexity and ensures readiness for immediate deployment or testing.

Inventive Principle:
Principle #10Preliminary action

3Ease of operation

If the measuring equipment is recovered by slowing the projectile in compacted bales backed by a sand trap, then recovery is achieved, but the sensitive measuring equipment is damaged

Engineering Contradiction:
Improverecovery processVSAvoidimpact damage to measuring equipment
Core Design Contradiction:
Ease of operationVSObject-affected harmful factors

Solution Approach 1:

The measuring equipment is extracted from the projectile body by detaching the payload container before recovery. The separated payload container with measuring equipment can be recovered independently using gentler methods (such as parachute deployment), avoiding the high-impact recovery process required for the full projectile and thus preventing damage to sensitive equipment.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The payload container is designed with protective features and separation mechanisms that cushion the measuring equipment before recovery. The separation occurs prior to the high-impact recovery phase, and the container itself provides protective cushioning during the recovery process, preventing damage to the embedded measuring equipment.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

4Strength

If the projectile body and payload container are permanently integrated, then structural integrity is improved, but the projectile cannot be modified between test and effect embodiments

Engineering Contradiction:
Improvestructural integrityVSAvoidembodiment flexibility
Core Design Contradiction:
StrengthVSAdaptability or versatility

Solution Approach 1:

The projectile is segmented into a reusable projectile body and a replaceable payload container connected by a separable interface. This segmentation maintains structural integrity of each component while enabling flexibility to swap payload containers between test and effect embodiments based on mission requirements.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The interface between the projectile body and payload container transitions from a static permanent connection to a dynamic separable connection. This allows the system to adapt its configuration dynamically - permanently integrated during a specific mission phase, then separable for reconfiguration to a different embodiment, providing both strength during operation and flexibility for modification.

Inventive Principle:
Principle #15Dynamics

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This approach enables safe recovery of measuring equipment without damage and simplifies the modification process, allowing the projectile to be efficiently converted between test and effect forms, ensuring cost-effectiveness and preventing disruptive interactions between the projectile body and effect charges.

Implementation Method 1

a separation charge arranged behind the payload container for separating the payload container from the projectile in the forward direction of the projectile

Methodology Applied
Scientific EffectExplosion: Explosion

Implementation Method 2

the separation charge consists of or comprises a propellant charge comprising a smokeless nitrocellulose propellant

Methodology Applied
Scientific EffectPropellant charge: Combustion

Implementation Method 3

the projectile comprises a pyrotechnic primer charge for initiating the propellant charge

Methodology Applied
Scientific EffectPyrotechnic primer charge: Detonation

Implementation Method 4

the payload container is connected to a parachute for recovery of the payload container after separation from the projectile

Methodology Applied
Scientific EffectParachute: Parachute

Implementation Method 5

the parachute is arranged and packed in a separable parachute container on or in the rear part of the payload container

Methodology Applied
Scientific EffectAerodynamic drag: Drag

Data Source

PatentUS11015907B2Method and arrangement for modifying a separable projectile
Publication Date: 2021.05.25 BAE SYSTEM BOFORS AB
  • US11015907B2 patent drawing

AI summary

A method for modifying a separable projectile between a test embodiment or an effect embodiment includes detaching the front projectile body from the rear projectile body, arranging a payload container in the front projectile body where the payload container comprises measuring equipment or an effect part, and fitting the front projectile body to the rear projectile body by way of a belt. A separable projectile which can be modified between a test embodiment and an effect embodiment is also provided.