Packaging and preservation of space-vehicle hardware Final report, 9 Jun. 1966 - 8 Jun. 1967
Packaging and preservation of space vehicle hardware
PRESERVATION↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Speed enhancement with soft computing hardware
We will review our work on electronic neural networks and evolvable hardware to bring out speed advantage.
soft computing neural networks evolvable hardware ↗
On two new trends in evolvable hardware: employment of HDL-based structuring, and design of multi-functional circuits
This paper comments on some directions of growth for evolvable hardware, proposes research directions that address the scalability problem and gives examples of results in novel areas approached by EHW.
evolvable hardware HDL polymorphic low-voltage↗
Hardware results of chaotic time series prediction using cascade error projection algorithm
This paper briefly describes an on-line hardware system based on 16x8x4 cascading neural network architecture.
prediction cascade error projection VLSI hardware ↗
EHWPACK: An evolvable hardware environment using the SPICE simulator and the Field Programmable Transistor Array
This paper describes the EHW development system, a tool that performs the evolutionary synthesis of electronic circuits, using the SPICE simulator and the Field Programmable Transistor Array hardware (FPTA) developed at JPL.
evolvable hardware spice simulations↗
Novel Highly Parallel and Systolic Architectures using Quantum Dot-Based Hardware
In this paper, we present novel parallel architectures based on Quantum-dot Cellular Automata (QCA) hardware.
Quantum-Dot Hardware Systolic Arrays Permutation M↗
A synthesis of engineering and business best-practices to achieve breakthroughs in flight hardware delivery
This paper discusses a synthesis of engineering and business best practices to achieve breakthroughs in flight hardware delivery.
flight hardware delivery↗
Reconfigurable Sensor Fusion Processing Hardware
The paper presents the concept and initial test from the hardware implementation of a low-power, high-speed reconfigurable sensor fusion processor.
Hardware implementation multisensor fusion data fu↗
Evolvable Hardware for Space Applications
This paper focuses on characteristics and applications of evolvable hardware (EHW) to space systems, and describes research directions and ongoing work at JPL.
Evolvable Hardware↗
Hardware QA: Preparing and Certifying a Rover to Land on the Surface of Mars
The Mars Science Laboratory Project presented multiple challenges of complexity for hardware QA personnel. Technical complexity was a major challenge. This is a one-of-kind never-before-been-built Spacecraft with a nuclear-powered Rover the size of a small SUV. It features a never-before-been-used Skycrane landing system featuring a Descent Stage which is a complex spacecraft within itself. Equally complex was figuring out how to support multiple activities at multiple facilities in this country and around the world at the same time.
technical challenges↗
Hardware and Software Engineering
The Launch Control System (LCS) is a part of the system used to launch the Space Launch System (SLS). It monitors and control of both vehicle and ground systems for SLS. My internship this spring was focused both on the hardware and software aspects of the command and control system. During my internship I worked in two groups, the Record and Playback Subsystem (RPS) and Kennedy Ground Control Subsystems (KGCS). During my time on RPS, I worked on automating the updating of displays and engineering reports. While on KGCS I worked on creating a power distribution diagram of the Control System Development Lab (CDL) and a new trainer for new interns or employees to gain an understanding of Programmable Logic Controllers (PLCs).
Hardware↗
A Systematic Approach to Hardware Qualification
A systematic approach for the development of a hardware qualification approach is described. This approach stems from the need to break the "Catch-22" of not being able to fly new technology because it hasn't flown. A physics of failure approach is used to identify failure modes and the impact and likelihood of these failures on the mission requirements is plotted in a Requirements Matrix. These same failure modes are plotted against the effectiveness of the available Preventions, Analyses, Control and Tests (PACTs) at screening for, or eliminating, these failure modes in a Test Effectiveness Matrix. Matrix multiplication results in a ranked set of PACTs which can be sorted according to cost and redundancy with other PACTs. This, and other information which results from the process, will allow project managers to make more informed decisions regarding the cost and risk tradeoffs inherent in any qualification program.
hardware↗
Extended Logic Intelligent Processing System for a Sensor Fusion Processor Hardware
The paper presents the hardware implementation and initial tests from a low-power, high-speed reconfigurable sensor fusion processor.
sensor↗
Global Tracking and Inventory of Military Hardware via LEO Satellite: A System Approach and Likely Scenario
A system for global inventory control of electronically tagged military hardware is achievable using a constellation of low earth orbit (LEO) satellites. Investigated are two proposed commercial LEO systems, both capable of providing global coverage but with dramatically different telecom capacities. This study is to verify the feasibility and performance of direct Tag-satellite communication.
global↗
Space-Hardware Design for Long Life With High Reliability
In 1991, the Cassini Project, NASA's planetary project to place a spacecraft in orbit about Saturn, funded a study at the Jet Propulsion Laboratory (JPL) to identify rules for design and test of hardware required to function reliably in space for very long lifetimes. Twenty-nine subjects were considered comprising 130 specific rules related to long-life issues such as accelerated life testing, cycling of mechanical devices, selection and application of parts, semiconductor junction temperatures, and worst-case analysis for long life. The study was subsequently published as a JPL document. One major conclusion of the workshop was that unattended space missions extending out to 25 years or more are feasible.
design↗
Ultrapure Water System at JSC for High Purity Cleaning of Flight Hardware, Astromaterial Handling Tools and Solar Wind Samples
Use of Ultrapure Water (UPW) for cleaning of astromaterial sample handling tools and containers was driven by the discontinuation of Freon 113 as a cleaning solvent, due to environmental concerns. Freon 113, recycled using distillation, was very effective at removing organic residues from sample handling hardware. The initial switch to high purity water for astromaterial tool cleaning was modeled after efforts at White Sands Test Facility (WSTF) and current semiconductor UPW production practices in the early 1990s. JSC curation’s first system was comprised of ion exchange polishing cylinders, 55 gallon PVDF-lined storage tank, a few tens of feet of PVDF piping, UV and particle filtration, and this system supported cleaning for lunar, meteorite and Cosmic Dust collectors lab operations. By 2000 a major expansion and upgrade was providing UPW of quality E-1 (ASTM D5127-90) or better at 10 gpm for cleaning of the Genesis solar wind payload for flight, in addition to sample handling tools for other astromaterials. This expansion included a 1000 gallon storage tank and several hundred feet of PVDF piping located in B. 31 and 31N. An extra reverse osmosis process unit was added to incoming water in 2005. Subsequently several major components were replaced, and in anticipation of adding new labs, an enlarged UPW system was designed in 2018 and completed in 2019. This system produces grade E1.1 UPW at 15 gpm in a continuous 1100 ft. loop with 5000 gal. storage tank, supplying 8 laboratories.
Ultrapure water↗
Modeling and Power-Hardware-in-the-Loop Validation of Synchronous Wind: An Inverterless Grid-Forming Wind Power Plant: Preprint
Grid-forming (GFM) control of Type-3 and Type-4 wind turbine generators has attracted substantial attention in power systems research; however, the limited over-current capability of power electronics converters continues to deteriorate the grid strength of the evolving power systems. Synchronous wind, also known as Type-5 wind turbine generator (WTG), offers a unique GFM solution to address grid integration and grid strength issues by keeping the grid largely synchronous at very high penetration levels of renewable generation. A Type-5 WTG interfaces to the electric grid via a synchronous generator (SG) driven by a variable-speed hydraulic torque converter; hence, the wind rotor operates in variable-speed mode for maximum power generation and the generator shaft remains synchronous to the grid. This paper developed and tested a high-fidelity model of Type-5 WTG under power-hardware-in-the-loop (PHIL) testing environment. The PHIL demonstration showed that a Type-5 WTGs inherently behaves as a GFM unit and can obtain similar performance in terms of power responses, wind rotor dynamics, and efficiency compared to Type-3 WTG in high wind conditions. The developed model also provides further insight on how Type-5 WTGs can benefit the smooth transition to power systems with high integration level of inverter-based resources.
grid strength↗
Poster: Hardware-Based Demonstration of Temperature Control Functions for Reactor Systems
Autonomous thermal regulation in nuclear reactors remains crucial for maintaining stable operation and ensuring the integrity of fuel. To alleviate public skepticism of the safety of nuclear reactors, demonstrating control over this key factor is pivotal. Utilizing electric heat pads to simulate the heat released in a reactor core, thermocouples for temperature monitoring, and an Arduino micro programmable logic controller (PLC) with an embedded proportional-integral-derivative (PID) algorithm for control, a hardware-based demonstration of a reactor heating system will validate the efficacy of reactor control over this key parameter.
21 - SPECIFIC NUCLEAR REACTORS AND ASSOCIATED PLAN↗