Tuesday, February 16, 2021

Fwd: Who Controls Space



Sent from my iPad

Begin forwarded message:

From: launchspace <info@launchspace.com>
Date: February 16, 2021 at 8:00:39 AM CST
To: Bobbygmartin1938@gmail.com
Subject: Who Controls Space
Reply-To: info@launchspace.com

February 16, 2021

 
(Launchspace Staff Writers)
 
Bethesda, MD – It is well known that the Straits of Gibraltar provide access to the Mediterranean Sea. In terms of strategic importance, this geographic phenomenon provides a control point for all seagoing traffic between the Atlantic Ocean and the Mediterranean Sea. Is there an analogous strategic structure for access to space?

For low-Earth orbit (LEO) traffic there is such a geographic phenomenon. Thanks to the physics of orbital mechanics, the equatorial plane offers the potential to act as an access-control point. The underlying reason is that all LEO traffic must cross the equator within every 50-minute time interval. This means that every satellite in every LEO constellation must cross the same plane twice per circuit around the Earth. If some entity were to place an offensive/defensive system in equatorial orbit, this could potentially control all near-Earth space operations. Such a concept could represent the foundation for a space-control architecture.

Imagine a scenario in which the US Space Force (USSF) might want to control all LEO operations. It is conceivable that one or more armed military space stations could be placed over the equator with crews that consist of USSF Guardians who operate a variety of onboard and ground-based weapons. Such vehicles could be equipped with docking ports to allow rendezvous and docking of other spacecraft for crew transfers and resupply activities.

Currently, there is only one fully operational and permanently inhabited space station in LEO, the International Space Station (ISS). This huge spacecraft is over 20 years old and is used to provide an orbiting facility for studying the effects of spaceflight on the human body and for conducting many long-length scientific studies. Because China, India, Russia and the US are planning other stations for the coming decades, space is already heavily contested by several spacefaring nations. There are already many adversarial operations in LEO and these seem to be intensifying. A primary mission of the USSF is to protect space assets and maintain US space superiority.

Equatorial orbits for space stations have not previously been considered. All prior space stations have been flown in orbits that cover most of the populated Earth. In other words, their orbits are inclined relative to the equatorial plane. The ISS is in an orbit that is inclined 51.6 degrees away from the equator. This orbital inclination was selected to accommodate Russian launch-site constraints while offering coverage of most populated areas. Without Russian participation the ISS orbit could have been inclined at 28.4 degrees, the latitude of the US launch site at Cape Canaveral. Unfortunately, the use of inclined orbits imposes certain limitations on launch timing and orbital operations as compared to equatorial destinations.

The use of an equatorial launch site would relieve certain constraints. For example, all spacecraft that are sent to the ISS have very narrow launch windows because liftoff can only occur as the launch site passes through the plane of the ISS orbit. If a planned launch window is missed, there is a one-day launch delay. A launch from an equatorial launch site to an equatorial space station can occur at any time because the launch site is always in the plane of the station. This geometrical convenience is also true for reusable transport vehicles, i.e., reentry will always bring the vehicle back to the equator.

A number of on-orbit operations can be simplified when operating in equatorial orbits. Maneuvering propellant is minimal because no plane changes are required for rendezvous and servicing of satellites. Rescue operations can be conducted at any time. On the adverse side, surveillance of the Earth's surface is limited to near-equator regions and launch operations would require an equatorial spaceport. Nevertheless, there may be important national security advantages for over-the-equator stations.



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Contact Launchspace for a quote: info@launchspace.com
Introduction to Space Systems Engineering
 
DURATION: THREE DAYS
LOCATION: LIVE/ONLINE
COURSE NO.: 1155
 
COURSE SUMMARY
This course acquaints both the engineer and support personnel with the meaning, terms used, techniques, advantages and challenges of Systems Engineering for space and related industries. The course deals with the systems approach, managing and successfully implementing a contract, program or project from inception through its life in the field. Each element in a program is taken from concept, definition and design, through fabrication, test and operation of the end product by addressing systems engineering techniques for each step. Topics include requirements identification and development, program planning and control, system design, system integration, risk management and cost controls.

COURSE MATERIALS:
Include extensive notes and reference materials.

WHO SHOULD ATTEND:
This introductory course addresses the major aspects of systems engineering and is directed toward a broad spectrum of company employees, ranging from the engineers beginning their careers to managers from specialty engineering design groups or functional support organizations - all of whom will benefit from knowledge of systems engineering techniques in performance of their job assignments. The course does not require graduate or undergraduate degrees.

WHAT YOU WILL LEARN:
This course teaches an engineering approach which emphasizes addressing all aspects of a system: its requirements, interfaces, cost constraints, design options and trade-off techniques for carrying out a successful program. The course highlights the importance of understanding, addressing and verifying requirements and how requirements must permeate every aspect of program activities. Functional Analysis/Functional Flow diagrams are introduced as a key method of addressing and verifying requirements. System design methods, sequences, trade studies and interfaces are then covered to follow a typical program progression. Supporting the analyses required in a design cycle are summarized along with explanation, examples and use of the "ilities" (reliability, availability, maintainability, etc.). The important aspects of proper program planning and control, cost estimating and cost containment, risk management and mitigation and the use of metrics to measure the performance and health of the program are also presented.

COURSE OUTLINE:

1..Introduction.
Review of recent space and aviation failures due to lack of Systems Engineering; What is Systems Engineering?

2..Requirements, Functional Analysis (FA) and Specifications.
Identification of requirement types (e.g., Functional, Performance, Operational, Test, Interface); how developed, allocated and verified. Introduction to FA; Functional Flow Diagrams; requirements-to-functions (methods, sequences); requirements implementation. Specification levels (System, Segment, Element, Subsystem, Component); Spec "Trees" ("A", "B" and "C" levels).

3..System Design.
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4..Program Planning and Control (PP&C).
Why PP&C is an important Systems Engineering Function; who does; management hints; tracking and measuring program performance; necessary Program Plans.

5..Trade Studies.
Methods/types; the trade study step-by-step decision process; generating alternative candidates; trade study "pitfalls"/cautions; KT (Kepner/Tregoe) method training.

6..Systems Integration and Systems Interfaces.
Integration tasks (e.g., defining, controlling, documenting, compatibility of, and verifying interfaces); other Interface/Integration activities (e.g., policies, schematics, Interface Working Groups, operations and schedules).

7..Operations (Ops) Analysis.
Ops requirements and analysis; Ops Concept and flow; allocating operations functions to hardware and procedures.

8..Compatibility Analysis.
Major types (electrical, mechanical, software/hardware interfaces); what to check; a "how to" outline; margin analyses.

9..The "'ilities".
Namely, Reliability, Availability, Maintainability, Human Factors/Human Engineering, Producability, Safety, Security, EMI/EMC; some "how-to's" of their use; cautions and risks.

10..Risk Management and Failure Modes & Effects Analysis (FMEA).
Risk identification, assessment, quantification (high, medium, low) and prioritization; risk handling techniques; Risk Mitigation Plans – their content and use; FMEA: what it is; basic analysis method(s); as part of Hazards Analysis.

11.Systems Analysis.
Types (e.g., program planning, ops profiles, system simulations, performance estimates, post-test comparisons); inputs required, sample tasks and expected outputs.

12..Metrics.
What they are; types (Product [Technical Performance Measures – TPM's] and Process metrics); use of; how to collect; goals and goal setting; cautions and guides.

13..Concurrent Engineering, Technical Quality Management (TQM) and Integrated Product Development (IPD).
What these are; why use (advantages)/how used; why they do/do not work; pros/cons of these three initiatives.

14..Costs/Cost Controls.
Cost terms; technical cost estimating and "pitfalls"; details of "Life-cycle" costs; what is a "Design-to-Cost" program and how to implement.

14..Engineering Plans and "Lessons Learned" Program.
Types of plans (e.g., Systems Engineering Management Plan, Master Program Plan, Configuration Management Plan, Software Development Plans, Safety Plans); typical contents; Collecting "lessons", documenting, distributing, using/non-use; 
problems with such a "program".

INSTRUCTOR:
Dr. GP Sandhoo has over 30 years of experience in spacecraft, systems, missiles and guided munitions. He leads the Spacecraft Engineering Division of the Naval Center of Space Technology (NCST) at the U.S. Naval Research Laboratory (NRL). He provides executive direction and technical leadership on new and advanced space systems and technologies. He previously worked at NASA's Johnson Space Center, Johns Hopkins University's Applied Physics Laboratory, and in industry. He holds a Bachelor's degree in mechanical engineering from the University of Maryland, a Master's degree in electrical engineering from Johns Hopkins University, Master's from the U.S. Naval War College, a Master's and a Doctorate in Aeronautics and Astronautics from George Washington University, and is a MIT Seminar XXI fellow. Currently, Sandhoo is a Captain in the U.S. Navy Reserve as an Engineering Duty Officer, and is qualified Space Cadre Officer (Space expert – VS8).

(202) 258-6133

Launchspace Training Courses
Here is a partial list of courses that we offer:
1040 Electromagnetic Environment Effects (E3) Testing
1050 Launch Vehicle and Spacecraft Acoustic Testing and Analysis
1060 Technologies and Systems for Space Debris Remediation
1125 Space Principles for Satellite and Launch Vehicle Professionals
1135 Space Vehicle Mechanisms: Elements of Successful Design
1136 Compliant Mechanism Design
1155 Introduction to Space Systems
2020 Orbital Mechanics & Cislunar Space Concepts
2022 Advanced Geostationary Orbital Mechanics
2035 Space Robotics: Design and Applications
2080 Spacecraft Avionics Systems Design and Applications
2100 Spacecraft Dynamics and Attitude Control
2110 Spacecraft Power System Design and Analysis
2200 Space Psychology: On-orbit and Cislunar Missions//Space Tourism
2210 Space Psychology: Lunar Missions//Space Tourism//Expeditions to Mars
3020 Satellite Communications
5010 Reusable Launch Vehicle Design, Systems and Operations
5030 Launch System Performance and Trajectory Design
5045 Launch Vehicle Environments, Loads and Testing for Compatibility
5046 Spacecraft Modal Testing
5060 Launch Vehicle Services Selection, Pricing, Contracting and Oversight
5070 Launch Vehicle Systems Design and Engineering
5075 Launch Vehicle Payload Integration
5080 Propulsion Systems for Launch Vehicles
5082 Propulsion Systems for Spacecraft
5085 Cryogenic Propulsion System Design
5090 Solid Rocket Motor Design and Applications
5095 Liquid Rocket Engine Design
5098 Advanced Liquid Rocket Engine Design Workshop
6000 Spaceport Fundamentals
6020 Space Mission Cost Estimation
6045 Spacecraft Program Management
6070 Facilitating Export Licensing of Space Systems

For more details on courses see the Launchspace Catalog on our website:
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LAUNCHSPACE is an educational and training organization dedicated to the continuing education of space professionals in support of the space community. 
We offer the largest array of customized, live client-site and online courses to government agencies and industry. Click on www.Launchspace.com to see our extensive catalog of course offerings. Any of these can be customized for your needs, or we can create a new course for you.
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