Streamlining a Critical Path to Lunar Settlement Kevin Hubbard,1 Linda T
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Project Selene: AIAA Lunar Base Camp
Project Selene: AIAA Lunar Base Camp AIAA Space Mission System 2019-2020 Virginia Tech Aerospace Engineering Faculty Advisor : Dr. Kevin Shinpaugh Team Members : Olivia Arthur, Bobby Aselford, Michel Becker, Patrick Crandall, Heidi Engebreth, Maedini Jayaprakash, Logan Lark, Nico Ortiz, Matthew Pieczynski, Brendan Ventura Member AIAA Number Member AIAA Number And Signature And Signature Faculty Advisor 25807 Dr. Kevin Shinpaugh Brendan Ventura 1109196 Matthew Pieczynski 936900 Team Lead/Operations Logan Lark 902106 Heidi Engebreth 1109232 Structures & Environment Patrick Crandall 1109193 Olivia Arthur 999589 Power & Thermal Maedini Jayaprakash 1085663 Robert Aselford 1109195 CCDH/Operations Michel Becker 1109194 Nico Ortiz 1109533 Attitude, Trajectory, Orbits and Launch Vehicles Contents 1 Symbols and Acronyms 8 2 Executive Summary 9 3 Preface and Introduction 13 3.1 Project Management . 13 3.2 Problem Definition . 14 3.2.1 Background and Motivation . 14 3.2.2 RFP and Description . 14 3.2.3 Project Scope . 15 3.2.4 Disciplines . 15 3.2.5 Societal Sectors . 15 3.2.6 Assumptions . 16 3.2.7 Relevant Capital and Resources . 16 4 Value System Design 17 4.1 Introduction . 17 4.2 Analytical Hierarchical Process . 17 4.2.1 Longevity . 18 4.2.2 Expandability . 19 4.2.3 Scientific Return . 19 4.2.4 Risk . 20 4.2.5 Cost . 21 5 Initial Concept of Operations 21 5.1 Orbital Analysis . 22 5.2 Launch Vehicles . 22 6 Habitat Location 25 6.1 Introduction . 25 6.2 Region Selection . 25 6.3 Locations of Interest . 26 6.4 Eliminated Locations . 26 6.5 Remaining Locations . 27 6.6 Chosen Location . -
2008 Estes-Cox Corp. All Rights Reserved
Estes-Cox Corp. 1295 H Street, P.O. BOX 227 Patent Pending Penrose, CO 81240-0227 ©2008 Estes-Cox Corp. All rights reserved. (9-08) PN 2927-8 TABLE OF CONTENTS HOW DO I START MY OWN ESTES ROCKET FLEET? The best way to begin model rocketry is with an Estes flying model rocket Starter Set or Launch Set. You can ® Index . .2 Skill Level 2 Rocket Kits . .30 either start with a Ready To Fly Starter Set or Launch Set that has a fully constructed model rocket or an E2X How To Start . .3 Skill Level 3 Rocket Kits . .34 Starter Set or Launch Set with a rocket that requires assembly prior to launching. Both types of sets come What to Know . .4 ‘E’ Engine Powered Kits . .36 complete with an electrical launch controller, adjustable launch pad and an information booklet to get you out Model Rocket Safety Code . .5 Blurzz™ Rocket Racers . .36 and flying in no time. Starter Sets include engines, Launch Sets let you choose your own engines (not includ- Ready To Fly Starter Sets . .6 How Model Rocket Engines Work . .38 ed). You’ll need four ‘AA’ alkaline batteries and perhaps glue, depending on which set you select. E2X® Starter Sets . .8 Model Rocket Engine Chart . .39 Ready to Fly Launch Sets . .10 Engine Time/Thrust Curves . .40 Launch Sets . .12 Model Rocket Accessories . .41 HOW EASY AND HOW MUCH TIME DOES IT TAKE TO BUILD MY ROCKETS? Ready To Fly Rockets . .14 Estes R/C Airplanes . .42 ® E2X Rocket Kits . .16 Estes Educator™ Products . -
The Messenger Spacecraft Power System Design and Early Mission Performance
THE MESSENGER SPACECRAFT POWER SYSTEM DESIGN AND EARLY MISSION PERFORMANCE G. Dakermanji, C. Person, J. Jenkins, L. Kennedy, D. Temkin Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Rd., Laurel, Maryland, 20723-6099, USA Email: [email protected] ABSTRACT The MESSENGER (MErcury Surface, Space ENvironment, GEochemistry, and Ranging) spacecraft was launched on August 3, 2004. The spacecraft will be inserted into Mercury orbit in March 2011 for one year of orbital operation. During the mission, the spacecraft distance to the Sun will vary between approximately 1 and 0.3 Astronomical Units (AU), imposing severe requirements on the spacecraft thermal and power systems design. The spacecraft is maintained behind a sunshade. The two single-axis, gimbaled solar array panels are designed to withstand the expected high temperatures. A peak power tracking system has been selected to allow operation over the widely varying solar array I-V curves. In order to reduce cost and risk while increasing the likelihood of mission success, the approach taken in the power system design, including the solar arrays, was to use conventional design, materials, and fabrication techniques. 1. MISSION DESCRIPTION a. Launch Configuration Sunshade MESSENGER (MErcury Surface, Space ENvironment, GEochemistry, and Ranging), shown in Fig. 1, is a Battery NASA Discovery Program spacecraft designed and built by the Johns Hopkins University Applied Physics Laboratory (APL). It will orbit the planet Mercury for one Earth year of orbital operation. Most of what is known about Mercury comes from the Mariner 10 spacecraft. Using three flybys, Mariner 10 was able to map about 45% of the planet surface during a one-year period between 1974 and 1975. -
Conceptual Human-System Interface Design for a Lunar Access Vehicle
Conceptual Human-System Interface Design for a Lunar Access Vehicle Mary Cummings Enlie Wang Cristin Smith Jessica Marquez Mark Duppen Stephane Essama Massachusetts Institute of Technology* Prepared For Draper Labs Award #: SC001-018 PI: Dava Newman HAL2005-04 September, 2005 http://halab.mit.edu e-mail: [email protected] *MIT Department of Aeronautics and Astronautics, Cambridge, MA 02139 TABLE OF CONTENTS 1 INTRODUCTION..................................................................................................... 1 1.1 THE GENERAL FRAMEWORK................................................................................ 1 1.2 ORGANIZATION.................................................................................................... 2 2 H-SI BACKGROUND AND MOTIVATION ........................................................ 3 2.1 APOLLO VS. LAV H-SI........................................................................................ 3 2.2 APOLLO VS. LUNAR ACCESS REQUIREMENTS ...................................................... 4 3 THE LAV CONCEPTUAL PROTOTYPE............................................................ 5 3.1 HS-I DESIGN ASSUMPTIONS ................................................................................ 5 3.2 THE CONCEPTUAL PROTOTYPE ............................................................................ 6 3.3 LANDING ZONE (LZ) DISPLAY............................................................................. 8 3.3.1 LZ Display Introduction................................................................................. -
Planning a Mission to the Lunar South Pole
Lunar Reconnaissance Orbiter: (Diviner) Audience Planning a Mission to Grades 9-10 the Lunar South Pole Time Recommended 1-2 hours AAAS STANDARDS Learning Objectives: • 12A/H1: Exhibit traits such as curiosity, honesty, open- • Learn about recent discoveries in lunar science. ness, and skepticism when making investigations, and value those traits in others. • Deduce information from various sources of scientific data. • 12E/H4: Insist that the key assumptions and reasoning in • Use critical thinking to compare and evaluate different datasets. any argument—whether one’s own or that of others—be • Participate in team-based decision-making. made explicit; analyze the arguments for flawed assump- • Use logical arguments and supporting information to justify decisions. tions, flawed reasoning, or both; and be critical of the claims if any flaws in the argument are found. • 4A/H3: Increasingly sophisticated technology is used Preparation: to learn about the universe. Visual, radio, and X-ray See teacher procedure for any details. telescopes collect information from across the entire spectrum of electromagnetic waves; computers handle Background Information: data and complicated computations to interpret them; space probes send back data and materials from The Moon’s surface thermal environment is among the most extreme of any remote parts of the solar system; and accelerators give planetary body in the solar system. With no atmosphere to store heat or filter subatomic particles energies that simulate conditions in the Sun’s radiation, midday temperatures on the Moon’s surface can reach the stars and in the early history of the universe before 127°C (hotter than boiling water) whereas at night they can fall as low as stars formed. -
Space Communications and Navigation (Scan) Testbed
National Aeronautics and Space Administration Space Communication and Navigation Testbed: Communications Technology for Exploration Richard Reinhart NASA Glenn Research Center July 2013 ISS Research and Development Conference Sponsored by Space Communication and Navigation Program Titan Lunar Neptune Relay Satellite Saturn Uranus Pluto LADEE Charon Jupiter Near Earth Optical Relay Pathfinder Mars NISNNISN MCC MOCs SCaN2023202520182015 Add: Services Provide: ••IntegratedEnhancedDeepIntegratedStandard Space service-basedServicesOptical Network Optical Initial Management Initial and architectureCapability Interfaces Capability (INM) ••SpaceDeepSpaceIntegratedDelay Space internetworking InternetworkingTolerant Service Optical Networking Execution Relay (DTN throughout Pathfinder and (ISE) IP) Solar Venus Deep Space ••InternationalLunarSystemSpaceDeep SpaceRelay Internetworking interoperability Satellite Antenna Initial Array Capability Antenna Optical Relay ••AssuredSignificantOpticalLunar Optical Ground safety Increases and Pathfinder Terminal security in Bandwidth (LADEE) of missions Array Pathfinder ••SignificantRetirementNearTDRS Earth K, L increases Optical of Aging Initial RFin bandwidth Systems Capability Sun Mercury • TDRSIncreased M,N microwave link data rates • Lunar Relay Payload (potential) 2 Microwave Links Optical Links NISN Next Generation Communication and Navigation Technology – Optical Communications – Antenna Arraying Technology – Receive and Transmit – Software Defined Radio – Advanced Antenna Technology – Spacecraft RF -
IT's a Little Chile up Here
IT’s A Little chile up here Press Kit | NET 29 July 2021 LAUNCH INFORMATION LAUNCH WINDOW ORBIT 12-day launch window opening from 29 July 2021 600km DAILY LAUNCH OPPORTUNITY The launch timing for this mission is the same for each day of the launch window. SATELLITES Time Zone Window Open Window Close NZT 18:00 20:00 UTC 06:00 08:00 1 EDT 02:00 04:00 PDT 23:00 01:00 The launch window extends for 12 days. INCLINATION 37 Degrees LAUNCH SITE Launch Complex 1, Mahia, New Zealand CUSTOMER LIVE STREAM Watch the live launch webcast: USSF rocketlabusa.com/live-stream Dedicated mission for U.S. Space Force 2 | Rocket Lab | Press Kit: It’s A Little Chile Up Here Mission OVERVIEW About ‘It’s a Little Chile Up Here’ Electron will launch a research and development satellite to low Earth orbit from Launch Complex 1 in New Zealand for the United States Space Force COMPLEX 1 LAUNCH MAHIA, NEW ZEALAND Electron will deploy an Air Force Research Laboratory- sponsored demonstration satellite called Monolith. ‘It’s a Little Chile Up Here’ The satellite will explore and demonstrate the use of a deployable sensor, where the sensor’s mass is a will be Rocket Lab’s: substantial fraction of the total mass of the spacecraft, changing the spacecraft’s dynamic properties and testing ability to maintain spacecraft attitude control. Analysis from the use of a deployable sensor aims to th st enable the use of smaller satellite buses when building 4 21 future deployable sensors such as weather satellites, launch for Electron launch thereby reducing the cost, complexity, and development timelines. -
Press Release
Rocket Lab, an End-to-End Space Company and Global Leader in Launch, to Become Publicly Traded Through Merger with Vector Acquisition Corporation End-to-end space company with an established track record, uniquely positioned to extend its lead across a launch, space systems and space applications market forecast to grow to $1.4 trillion by 2030 One of only two U.S. commercial companies delivering regular access to orbit: 97 satellites deployed for governments and private companies across 16 missions Second most frequently launched U.S. orbital rocket, with proven Photon spacecraft platform already operating on orbit and missions booked to the Moon, Mars and Venus Transaction will provide capital to fund development of reusable Neutron launch vehicle with an 8-ton payload lift capacity tailored for mega constellations, deep space missions and human spaceflight Proceeds also expected to fund organic and inorganic growth in the space systems market and support expansion into space applications enabling Rocket Lab to deliver data and services from space Business combination values Rocket Lab at an implied pro forma enterprise value of $4.1 billion. Pro forma cash balance of the combined company of approximately $750 million at close Rocket Lab forecasts that it will generate positive adjusted EBITDA in 2023, positive cash flows in 2024 and more than $1 billion in revenue in 2026 Group of top-tier institutional investors have committed to participate in the transaction through a significantly oversubscribed PIPE of approximately $470 million, with 39 total investors including Vector Capital, BlackRock and Neuberger Berman Transaction is expected to close in Q2 2021, upon which Rocket Lab will be publicly listed on the Nasdaq under the ticker RKLB Current Rocket Lab shareholders will own 82% of the pro forma equity of combined company Long Beach, California – 1 March 2021 – Rocket Lab USA, Inc. -
2019 Nano/Microsatellite Market Forecast, 9Th Edition
2019 NANO/MICROSATELLITE MARKET FORECAST, 9TH EDITION Copyright 2018, SpaceWorks Enterprises, Inc. (SEI) APPROVED FOR PUBLIC RELEASE. SPACEWORKS ENTERPRISES, INC., COPYRIGHT 2018. 1 Since 2008, SpaceWorks has actively monitored companies and economic activity across both the satellite and launch sectors 0 - 50 kg 50 - 250kg 250 - 1000kg 1000 - 2000kg 2000kg+ Custom market assessments are available for all mass classes NANO/MICROSATELLITE DEFINITION Picosatellite Nanosatellite Microsatellite Small/Medium Satellite (0.1 – 0.99 kg) (1 – 10 kg) (10 – 100 kg) (100 – 1000 kg) 0 kg 1 kg 10 kg 100 kg 1000 kg This report bounds the upper range of interest in microsatellites at 50 kg given the relatively large amount of satellite development activity in the 1 – 50 kg range FORECASTING METHODOLOGY SpaceWorks’ proprietary Launch Demand Database (LDDB) Downstream serves as the data source for all satellite market Demand assessments ▪ Planned The LDDB is a catalogue of over 10,000+ historical and Constellations future satellites containing both public and non-public (LDDB) satellite programs Launch Supply SpaceWorks newly updated Probabilistic Forecast Model (PFM) is used to generate future market potential SpaceWorks PFM Model ▪ The PFM considers down-stream demand, announced/planed satellite constellations, and supply-side dynamics, among other relevant factors Expert Analysis The team of expert industry analysts at SpaceWorks SpaceWorks further interprets and refines the PFM results to create Forecast accurate market forecasts Methodology at a Glance 2018 SpaceWorks forecasted 2018 nano/microsatellite launches with unprecedented accuracy – actual satellites launched amounted to just 5% below our analysts’ predictions. In line with SpaceWorks’ expectations, the industry corrected after a record launch year in 2017, sending 20% less nano/microsatellites to orbit than in 2018. -
588168 Amendment No. 56 NASA Glenn Research Center, License
NRC FORM 374 PAGE 1 OF 7 PAGES U.S. NUCLEAR REGULATORY COMMISSION Amendment No. 56 MATERIALS LICENSE Pursuant to the Atomic Energy Act of 1954, as amended, the Energy Reorganization Act of 1974 (Public Law 93-438), and Title 10, Code of Federal Regulations, Chapter I, Parts 30, 31, 32, 33, 34, 35, 36, 37, 39, 40, 70 and 71, and in reliance on statements and representations heretofore made by the licensee, a license is hereby issued authorizing the licensee to receive, acquire, possess, and transfer byproduct, source, and special nuclear material designated below; to use such material for the purpose(s) and at the place(s) designated below; to deliver or transfer such material to persons authorized to receive it in accordance with the regulations of the applicable Part(s). This license shall be deemed to contain the conditions specified in Section 183 of the Atomic Energy Act of 1954, as amended, and is subject to all applicable rules, regulations, and orders of the Nuclear Regulatory Commission now or hereafter in effect and to any conditions specified below. Licensee In accordance with letter dated 4. Expiration Date: March 31, 2025 March 28, 201 1. National Aeronautics & Space Administration R John H. Glenn Research Center 5. Docket No.: 030-05626 2. 21000 Brookpark Road Reference No.: Mailstop 6-4 Cleveland, OH 44135 6. Byproduct, source, 9. Authorized use and/or special nuclear material A. Any byproduct material A. Activation ~ucts A. For research and development as between atomic numbers described in 10 CFR 30.4. Possession 3 and 83 incident to the radiological characterization surveys of a shut-down cyclotron. -
Concept for a Crewed Lunar Lander Operating from the Lunar Orbiting Platform-Gateway
69th International Astronautical Congress (IAC), Bremen, Germany, 1-5 October 2018. Copyright © 2018 by Lockheed Martin Corporation. Published by the IAF, with permission and released to the IAF to publish in all forms. IAC-18.A5.1.4x46653 Concept for a Crewed Lunar Lander Operating from the Lunar Orbiting Platform-Gateway Timothy Cichana*, Stephen A. Baileyb, Adam Burchc, Nickolas W. Kirbyd aSpace Exploration Architect, P.O. Box 179, MS H3005, Lockheed Martin Space, Denver, Colorado, U.S.A. 80201, [email protected] bPresident, 8100 Shaffer Parkway, Unit 130, Deep Space Systems, Inc., Littleton, Colorado, 80127-4124, [email protected] cDesign Engineer / Graphic Artist, 8341 Sangre de Christo Rd, Deep Space Systems, Inc., Littleton, Colorado, 80127, [email protected] dSystems Engineer, Advanced Programs, P.O. Box 179, MS H3005, Lockheed Martin Space, Denver, Colorado, U.S.A. 80201, [email protected] * Corresponding Author Abstract Lockheed Martin is working with NASA on the development of the Lunar Orbiting Platform – Gateway, or Gateway. Positioned in the vicinity of the Moon, the Gateway allows astronauts to demonstrate operations beyond Low Earth Orbit for months at a time. The Gateway is evolvable, flexible, modular, and is a precursor and mission demonstrator directly on the path to Mars. Mars Base Camp is Lockheed Martin's vision for sending humans to Mars. Operations from an orbital base camp will build on a strong foundation of today's technologies and emphasize scientific exploration as mission cornerstones. Key aspects of Mars Base Camp include utilizing liquid oxygen and hydrogen as the basis for a nascent water-based economy and the development of a reusable lander/ascent vehicle. -
10 Things to Know About NASA's Glenn Research Center
National Aeronautics and Space Administration 10 Things to Know About NASA’s Glenn Research Center 1. NASA Glenn’s economic impact in Ohio exceeds $1.4 billion per year. According to an economic impact study by Cleveland State University’s Center for Economic Development, Glenn generates over $700 million annually in economic activity and creates over 7,000 jobs. NASA Glenn also generates nearly $500 million in labor income and approximately $120 million in tax revenue per year. 2. Glenn scientists and engineers are prolific inventors. The research center holds more than 725 patents and has won over 120 R&D 100 Awards, also known as the Oscars of innovation. That’s more than any other NASA center. Glenn strives to increase private sector revenue and contribute to private sector job growth by licensing its inventions. 3. Every U.S. aircraft has NASA Glenn technology on board. NASA is with you when you fly. Today’s commercial airliners are safer, quieter and more fuel efficient because of NASA Glenn technology. Glenn advancements such as ice detection and air traffic control systems have made flying safer. Glenn jet engine combustors have resulted in more efficient aircraft engines, and Glenn developed nozzle chevrons are used to make the Boeing 787 Dreamliner and new 737 MAX quieter. 4. Glenn is transforming aviation by developing revolutionary technologies for aircraft and the national airspace system. Glenn is working to dramatically improve efficiency, reduce costs and noise, and maintain safety in crowded skies. The center leads the agency’s effort to develop hybrid electric propulsion systems for commercial passenger aircraft.