Deployable Rocket Camera for External Spaceflight Imaging

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Solution Overview

Problem

Photography during spaceflight is challenging due to the limitations of land-based cameras and onboard cameras, which struggle with distortion, distance, and inability to capture detailed images or videos of spacecraft and astronauts.

Innovation Solution

An autonomous deployable camera (ADC) system that captures images and videos during spaceflight, autonomously lands after separation from the spacecraft, and can transmit or store data for recovery, with features like a parachute for landing and tracking devices for retrieval.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If land-based cameras are used to photograph rocket launches, then images can be captured from ground level, but the images are distorted due to atmospheric refraction and lack detail at higher altitudes

Engineering Contradiction:
Improveimage qualityVSAvoiddistance from rocket trajectory
Core Design Contradiction:
Measurement precisionVSLength of moving object

Solution Approach 1:

The camera system is divided into separable components including the camera module, parachute deployment mechanism, and recovery system. The camera can be deployed as an independent unit from the rocket, allowing it to reach optimal positioning distances for clear photography without being constrained by ground-based limitations or rocket-mounted space constraints.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A parachute system acts as an intermediary mechanism between the camera deployment and ground recovery. The parachute enables controlled descent of the camera to a safe landing zone, serving as the mediator that connects the aerial photography mission with ground-based recovery operations.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Adaptability or versatility

If cameras are mounted on the rocket, then close-up images can be captured, but the camera cannot capture external views of the spacecraft and astronauts from outside

Engineering Contradiction:
Improveviewing angleVSAvoidcamera deployment system
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The camera system transitions from a static ground-based position to a dynamic deployed position near the rocket trajectory. The camera is released at a specific altitude and uses parachute control to maintain optimal positioning, enabling dynamic adjustment of viewing angles to capture both external spacecraft views and close-up details.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The camera operates in a third dimension by being deployed to fly alongside the rocket trajectory rather than remaining on the ground or fixed to the rocket. This dimensional transition allows the camera to achieve optimal positioning for capturing external views of the spacecraft and astronauts from multiple angles.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

3Reliability

If a parachute is deployed to slow descent, then the camera can land safely, but the parachute adds weight and complexity to the system

Engineering Contradiction:
Improvesafe landingVSAvoidcamera system weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The parachute system is designed as a disposable component that is deployed only during the descent phase and then discarded after the camera lands. This approach allows the camera to have safe landing capability without permanently carrying the weight and complexity of the parachute system throughout the entire mission.

Inventive Principle:
Principle #34Discarding and recovering

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

Enables high-quality imagery of spacecraft and astronauts in microgravity, providing commercially valuable footage without requiring real-time telemetry, and ensuring safe separation and retrieval of the camera.

Implementation Method 1

The ADC may include a parachute to slow the descent of the ADC

Methodology Applied
Scientific EffectAir resistance: Drag

Data Source

PatentUS12618652B2Rocket camera system and method with rocket and camera dispenser
Publication Date: 2026.05.05 BLUE ORIGIN MANUFACTURING LLC
  • US12618652B2 patent drawing
  • US12618652B2 patent drawing
  • US12618652B2 patent drawing

AI summary

Systems and methods for photography of a spacecraft during space flight are provided. An autonomous deployable camera (ADC) is configured to capture images and video of a portion of a rocket, such as a crew capsule, as it flies in space with the Earth's horizon in the background and astronauts within the crew capsule visible and recognizable through windows of the crew capsule. The ADC, being reusable, is configured to land on the ground independent of landings or flight trajectories of the crew capsule or other parts of a rocket. The ADC includes a parachute to slow the descent of the ADC and tracking hardware to allow the ADC to be relatively easily recovered on the ground. After recovery, images are downloadable from the ADC.