Payload USER's GUIDE
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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 . -
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. -
Launcherone Success Opens New Space Access Gateway Guy Norris January 22, 2021
1/22/21 7:05 1/6 LauncherOne Success Opens New Space Access Gateway Guy Norris January 22, 2021 With San Nicolas Island far below, LauncherOne headed for polar orbit. Credit: Virgin Orbit Virgin Orbit had barely tweeted news of the successful Jan. 17 space debut of its LauncherOne vehicle on social media when new launch contracts began arriving in the company’s email inbox. A testament to the pent-up market demand for small-satellite launch capability, the speedy reaction to the long-awaited demonstration of the new space-access vehicle paves the way for multiple follow-on Virgin Orbit missions by year-end and a potential doubling of the rate in 2022. First successful privately developed air-launched, liquid-fueled rocket Payloads deployed for NASA’s Venture Class Launch Services program The glitch-free !ight of LauncherOne on its second demonstration test was a critical and much-welcomed milestone for the Long Beach, California-based company. Coming almost nine years a"er the air-launch concept was #rst unveiled by Virgin founder Richard Branson, and six years a"er the start of full-scale development, the !ight followed last May’s #rst demonstration mission, which ended abruptly when the rocket motor shut o$ a"er just 4 sec. 1/22/21 7:05 2/6 A"er an exhaustive analysis and modi#cations to beef up the oxidizer feed line at the heart of the #rst !ight failure, the path to the Launch Demo 2 test was then delayed until January 2021 by the COVID-19 pandemic. With the LauncherOne system now proven, design changes veri#ed and the #rst 10 small satellites placed in orbit, Virgin Orbit is already focusing on the next steps to ramp up its production and launch-cadence capabilities. -
Cubesat Mission: from Design to Operation
applied sciences Article CubeSat Mission: From Design to Operation Cristóbal Nieto-Peroy 1 and M. Reza Emami 1,2,* 1 Onboard Space Systems Group, Department of Computer Science, Electrical and Space Engineering, Luleå University of Technology, Space Campus, 981 92 Kiruna, Sweden 2 Aerospace Mechatronics Group, University of Toronto Institute for Aerospace Studies, Toronto, ON M3H 5T6, Canada * Correspondence: [email protected]; Tel.: +1-416-946-3357 Received: 30 June 2019; Accepted: 29 July 2019; Published: 1 August 2019 Featured Application: Design, fabrication, testing, launch and operation of a particular CubeSat are detailed, as a reference for prospective developers of CubeSat missions. Abstract: The current success rate of CubeSat missions, particularly for first-time developers, may discourage non-profit organizations to start new projects. CubeSat development teams may not be able to dedicate the resources that are necessary to maintain Quality Assurance as it is performed for the reliable conventional satellite projects. This paper discusses the structured life-cycle of a CubeSat project, using as a reference the authors’ recent experience of developing and operating a 2U CubeSat, called qbee50-LTU-OC, as part of the QB50 mission. This paper also provides a critique of some of the current poor practices and methodologies while carrying out CubeSat projects. Keywords: CubeSat; miniaturized satellite; nanosatellite; small satellite development 1. Introduction There have been nearly 1000 CubeSats launched to the orbit since the inception of the concept in 2000 [1]. An up-to-date statistics of CubeSat missions can be found in Reference [2]. A summary of CubeSat missions up to 2016 can also be found in Reference [3]. -
Redalyc.Status and Trends of Smallsats and Their Launch Vehicles
Journal of Aerospace Technology and Management ISSN: 1984-9648 [email protected] Instituto de Aeronáutica e Espaço Brasil Wekerle, Timo; Bezerra Pessoa Filho, José; Vergueiro Loures da Costa, Luís Eduardo; Gonzaga Trabasso, Luís Status and Trends of Smallsats and Their Launch Vehicles — An Up-to-date Review Journal of Aerospace Technology and Management, vol. 9, núm. 3, julio-septiembre, 2017, pp. 269-286 Instituto de Aeronáutica e Espaço São Paulo, Brasil Available in: http://www.redalyc.org/articulo.oa?id=309452133001 How to cite Complete issue Scientific Information System More information about this article Network of Scientific Journals from Latin America, the Caribbean, Spain and Portugal Journal's homepage in redalyc.org Non-profit academic project, developed under the open access initiative doi: 10.5028/jatm.v9i3.853 Status and Trends of Smallsats and Their Launch Vehicles — An Up-to-date Review Timo Wekerle1, José Bezerra Pessoa Filho2, Luís Eduardo Vergueiro Loures da Costa1, Luís Gonzaga Trabasso1 ABSTRACT: This paper presents an analysis of the scenario of small satellites and its correspondent launch vehicles. The INTRODUCTION miniaturization of electronics, together with reliability and performance increase as well as reduction of cost, have During the past 30 years, electronic devices have experienced allowed the use of commercials-off-the-shelf in the space industry, fostering the Smallsat use. An analysis of the enormous advancements in terms of performance, reliability and launched Smallsats during the last 20 years is accomplished lower prices. In the mid-80s, a USD 36 million supercomputer and the main factors for the Smallsat (r)evolution, outlined. -
A Breath of Fresh Air: Air-Scooping Electric Propulsion in Very Low Earth Orbit
A BREATH OF FRESH AIR: AIR-SCOOPING ELECTRIC PROPULSION IN VERY LOW EARTH ORBIT Rostislav Spektor and Karen L. Jones Air-scooping electric propulsion (ASEP) is a game-changing concept that extends the lifetime of very low Earth orbit (VLEO) satellites by providing periodic reboosting to maintain orbital altitudes. The ASEP concept consists of a solar array-powered space vehicle augmented with electric propulsion (EP) while utilizing ambient air as a propellant. First proposed in the 1960s, ASEP has attracted increased interest and research funding during the past decade. ASEP technology is designed to maintain lower orbital altitudes, which could reduce latency for a communication satellite or increase resolution for a remote sensing satellite. Furthermore, an ASEP space vehicle that stores excess gas in its fuel tank can serve as a reusable space tug, reducing the need for high-power chemical boosters that directly insert satellites into their final orbit. Air-breathing propulsion can only work within a narrow range of operational altitudes, where air molecules exist in sufficient abundance to provide propellant for the thruster but where the density of these molecules does not cause excessive drag on the vehicle. Technical hurdles remain, such as how to optimize the air-scoop design and electric propulsion system. Also, the corrosive VLEO atmosphere poses unique challenges for material durability. Despite these difficulties, both commercial and government researchers are making progress. Although ASEP technology is still immature, it is on the cusp of transitioning between research and development and demonstration phases. This paper describes the technical challenges, innovation leaders, and potential market evolution as satellite operators seek ways to improve performance and endurance. -
The Aerospace Update
The Aerospace Update Hubble’s Cartwheel Jan 25, 2018 Image Credit: ESA/Hubble&NASA U.S. Military Satellite Launched to Fortify Against Missile Attacks A billion-dollar U.S. military satellite rode a United Launch Alliance Atlas 5 rocket into orbit Friday, Jan 19th night from Cape Canaveral, joining a network of space sentinels warning of threatening missile launches from North Korea, or any other place on the globe. Lockheed Martin, builder of the SBIRS GEO Flight 4 spacecraft, said ground controllers with the Air Force’s 460th Space Wing established contact with the newly-launched satellite soon after its release from the Atlas 5’s Centaur upper stage. Video Source: ULA Source: Stephen Clark @ SpaceFlightNow.com “Bell Ringer to a Launch Anywhere on the Face of the Planet” The $1.2 billion SBIRS GEO Flight 4 satellite launched aboard the Atlas 5 rocket will finish the initial deployment of the Air Force’s new-generation missile- warning network. When complete, the constellation that will include a minimum of four SBIRS craft stationed in geosynchronous orbit and at least two infrared payloads in elliptical orbits aboard top secret National Reconnaissance Office spy satellites, providing polar coverage. The SBIRS fleet is the “bell ringer to a launch anywhere on the face of the planet,” said Col. Dennis Bythewood, director of the remote sensing systems directorate at the Air Force’s Space and Missile Systems Center. Source: Stephen Clark @ SpaceFlightNow.com Photo Credit: Lockheed Martin Rocket Lab Electron Reaches Orbit on Second Launch Rocket Lab’s commercial Electron launcher named “Still Testing” soared into orbit from New Zealand on Saturday, Jan 20th U.S. -
IUS/TUG ORBITAL OPERATIONS and MISSION SUPPORT STUDY FINAL REPORT
https://ntrs.nasa.gov/search.jsp?R=19750016720 2020-03-22T21:57:01+00:00Z Prepared for the MAY, 1975 GEORGE C MARSHALL SPACE FLIGHT CENTER Contract No NAS8-31009 Huntsville, Alabama IBM No 75W-00072 IUS/TUG ORBITAL OPERATIONS and MISSION SUPPORT STUDY FINAL REPORT Vol V of V - Cost Estimates (NASA-CR-143857) TUS/TUG ORBITAL OPEFATIONS N75-24792 AND M-ISSION SUPPORT STUDY. VOLUME 5: COST ESTI ATES Final Report (Internattonal Business Machines Corp.) 184 p HC $7.00 Unclas CSCL 22A G3/13 26227 Prepared for the MAY, 1975 GEORGE C MARSHALL SPACE FLIGHT CENTER Contract No NAS8-31009 Huntsville, Alabama IBM No 75W-00072 IUS/TUG ORBITAL OPERATIONS and MISSION SUPPORT STUDY FINAL REPORT Vol V of V - Cost Estimates Classification and Content Approval - '- Data Manager Approval Z2 Program Office Approval zC7 !4 PHILCO 490 Phico Fcrd Corporation Federal Systems Division, Space Systems/Huntsville, AlabmaWestr eopme Laorories son FOREWORD This final report of the IUS/Tug Orbital Operations and Mission Study was prepared for the National Aeronautics and Space Administration, George C Marshall Space Flight Center by the IBM Corporation in accordance with Contract NAS8-31009 The study effort described herein was conducted under the direction of NASA Contract Officer's Representative (COR), Mr. Sidney P Saucier This report was prepared by the IBM Corporation, Federal Systems Division, Huntsville, Alabama, under the direction of Mr Roy E Day, IBM Study Manager Technical support was provided to IBM by the Philco-Ford Corporation, Western Development Laboratories Division, Palo Alto, California, under the direction of Dr W E Waters, Philco-Ford Study Manager The study results were developed during the period from dune, 1974, through February, 1975, with the final report being distributed in May, 1975. -
George C. Marshall Space Flight Center Malshall Space Flight Center, Alabama
NASA TECHNICAL MEMORANDUM NASA TM X-53973 SPACE FLIGHT EVOLUTION By Georg von Tiesenhausen and Terry H. Sharpe Advanced Systems Analysis Office June 30,1970 NASA George C. Marshall Space Flight Center Malshall Space Flight Center, Alabama MSFC - Form 3190 (September 1968) j NASA TM X-53973 I [. TITLE AND SUBTITLE 5. REPORT DATE June 30,1970 Space Flight Evolution 6. PERFORMlNG ORGANIZATION CODE PD-SA 7. AUTHOR(S) 8. PERFORMING ORGANIZATION REPORT # Georg von Tiesenhausen and Terry H. Sharpe I 3. PERFORMlNG ORGANIZATION NAME AND ADDRESS lo. WORK UNIT, NO. Advanced Systems Analysis Office Program Development 1 1. CONTRACT OR GRANT NO. Marshall Space Flight Center, Alabama 35812 13. TYPE OF REPORT & PERIOD COVEREC 2. SPONSORING AGENCY NAME AND ADDRESS Technical Memorandum 14. SPONSORING AGENCY CODE I 15. SUPPLEMENTARY NOTES 16. ABSTRACT This report describes a possible comprehensive path of future, space flight evolution. The material in part originated from earlier NASA efforts to defme a space program in which earth orbital, lunar, and planetary programs are integrated. The material presented is not related to specific time schedules but provides an evolutionary sequence. The concepts of commonality of hardware and reusability of systems are introduced as keys to a low cost approach to space flight. The verbal descriptions are complemented by graphic interpretations in order to convey a more vivid impression of the concepts and ideas which make upthis program. 17. KEY WORDS 18. DISTRIBUTION STATEMENT STAR Announcement Advanced Systems Analysis Office 19. SECURITY CLASSIF. (of this rePmt> (20. SECURITY CLA ;IF. (of this page) 121. NO. OF PAGES 122. -
Increasing Launch Rate and Payload Capabilities
Aerial Launch Vehicles: Increasing Launch Rate and Payload Capabilities Yves Tscheuschner1 and Alec B. Devereaux2 University of Colorado, Boulder, Colorado Two of man's greatest achievements have been the first flight at Kitty Hawk and pushing into the final frontier that is space. Air launch systems aim to combine these great achievements into a revolutionary way to deliver satellites, cargo and eventually people into space. Launching from an aircraft has many advantages, including the ability to launch at any inclination and from above bad weather, which could delay ground launches. While many concepts for launching rockets from an airplane have been developed, very few have made it past the drawing board. Only the Pegasus and, to a lesser extent, SpaceShipOne have truly shown the feasibility of such a system. However, a recent push for rapid, small payload to orbit launches by the military and a general need for cheaper, heavy lift options are leading to an increasing interest in air launch methods. In order for the efficiency and flexibility of the system to be realized, however, additional funding and research are necessary. Nomenclature ALASA = airborne launch assist space access ALS = air launch system DARPA = defense advanced research project agency LEO = low Earth orbit LOX = liquid oxygen RP-1 = rocket propellant 1 MAKS = Russian air launch system MECO = main engine cutoff SS1 = space ship one SS2 = space ship two I. Introduction W hat typically comes to mind when considering launching people or satellites to space are the towering rocket poised on the launch pad. These images are engraved in the minds of both the public and scientists alike.