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Tuesday, July 28, 2020 | History

2 edition of Vehicle/payload interface specification for the Reusable Reentry Satellite found in the catalog.

Vehicle/payload interface specification for the Reusable Reentry Satellite

Vehicle/payload interface specification for the Reusable Reentry Satellite

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  • 33 Currently reading

Published by SAIC, National Aeronautics and Space Administration, National Technical Information Service, distributor in Torrance, Calif, [Washington, DC, Springfield, Va .
Written in English

    Subjects:
  • Artificial satellites -- Atmospheric entry.

  • Edition Notes

    Statementprepared by Science Applications International Corporation.
    Series[NASA contractor report] -- NASA CR-187883.
    ContributionsUnited States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Paginationi, 14 [3] p.
    Number of Pages14
    ID Numbers
    Open LibraryOL14689687M

    An illustration of an open book. Books. An illustration of two cells of a film strip. Video An illustration of an audio speaker. The overall Reusable Reentry Satellite (RRS) Phase B Study objective is to design a relatively inexpensive satellite to access space for extended periods of time, with eventual recovery of experiments on Earth. Falcon 9 is a partially reusable two-stage-to-orbit medium-lift launch vehicle designed and manufactured by SpaceX in the United States. It is powered by Merlin engines, also developed by SpaceX, burning cryogenic liquid oxygen and rocket-grade kerosene as name is derived from the fictional Star Wars spacecraft, the Millennium Falcon, and the nine Merlin engines of the rocket's.

    The Falcon Heavy is a partially reusable heavy-lift launch vehicle designed and manufactured by is derived from the Falcon 9 vehicle and consists of a strengthened Falcon 9 first stage as the center core with two additional Falcon 9-like first stages as strap-on boosters. The Falcon Heavy has the highest payload capacity of any currently operational launch vehicle, the third-highest.   Return of the two reusable stages to the launch site is to be assured for any feasible option. The SpaceLiner Orbiter reentry has been simulated with an entry interface speed of approximately km/s. Reaching its once-around destination CSG in Kourou is without problem for the orbiter due to its very good hypersonic L/D well above 2.

    Payload Interface Guide for The Pegasus Air-Launched Space Booster by Marty Mosier* and Gary Harris** Orbital Sciences Corporation ABSTRACT The Pegasus tm Air-Launched Space Booster combines an innovative approach to satellite launch operations with the latest in proven launch vehicle technology. Pegasus provides small. The SpaceX Dragon, also known as Dragon 1 or Cargo Dragon, was a class of reusable cargo spacecraft developed by SpaceX, an American private space transportation was launched into orbit by the company's Falcon 9 launch vehicle to resupply the International Space Station (ISS). It is now superseded by SpaceX Dragon During its maiden flight in December , Dragon .


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Vehicle/payload interface specification for the Reusable Reentry Satellite Download PDF EPUB FB2

G's. The initial Reusable Reentry Vehicle/Payload Module (RRV/PM) integration and checkout will occur at the launch base unless otherwise agreed to in a mission-unique addendum to this specification. Pre-integration interface qualification shall be done using emulators as described below.

The RRS consists of a: a) Vehicle Segment. Get this from a library. Vehicle/payload interface specification for the Reusable Reentry Satellite. [United States. National Aeronautics and Space Administration.;].

This document describes the common interface requirements between the Vehicle Segment and the Payload Segment of the Reusable Reentry Satellite (RRS) system. The system consists of a single transport vehicle design that provides a uniform, unidirectional payload gravitational environment which is selectable during on-orbit operations over the range of 10(exp -5) (microgravity) to g's.

This Interface Specification (IFS) identifies, defines, and controls the interface between the Reusable Reentry Satellite (RRS) Vehicle (RRV) Experiment Module (EM) and the Support Module (SM) equipment. Contained in this specification are the physical, functional, and environmental interface requirements for the SM and EM.

The RRS System Specification document organization is shown schematically. The RRS Vehicle (RRV), Payload Module (PM), and the Operations Support (OS) are the three main segments of the overall system for which formal interface control will exist.

The number and relationship of these interface specifications to the main segments is also shown. requirements for the Reusable Reentry Satellite (RRS) system. The RRS System Specification consists of a Rodent Module (RM) Segment, a Reusable Reentry Vehicle (RRV) Segment, and an Operations Support (OS) Segment.

The segment specifications and associated interface specifications are contained in Volumes of the RRS System Specification. This specification establishes the performance, design, development, and test requirements for the Reusable Reentry Satellite (RRS) Rodent Module (RM)., APPLICABLE DOCUMENTS As specified in RRS-SS, paragraph REQUIREMENTS SYSTEM DEFINITION The RRS System is composed of the Payload Segment (PS).

Audio Books & Poetry Community Audio Computers, Technology and Science Music, Arts & Culture News & Public Affairs Non-English Audio Spirituality & Religion. Librivox Free Audiobook. DJGAME Fragancia Shampoo LobaMAISCruel's Podcast Fritz Kalkbrenner-Podcast BonKoze Dlo, Asenisman Ak Fatra Aarathy Elangovan Salud.

In addition, Boeing is the prime contractor for the XB Orbital Test Vehicle, the newest and most advanced unmanned re-entry spacecraft used by the U.S. Air Force to perform risk-reduction and experimentation for reusable space vehicle technologies.

The PCM is capable of holding 3,kg of cargo for disposal via destructive re-entry. Service Module Photo: Orbital ATK. Located in the aft section of the spacecraft, the Cygnus Service Module provides power generation & storage, vehicle control, propulsion, guidance and the Grapple Fixture for the Station’s robotic arm.

Outline for reusable reentry satellite system specification, volumes 1 - volume 9. Abstract. This document describes the outline proposed by the SAIC team for the RRS System Specification document. This document will be updated periodically during the course of the study, providing design insights and information pertinent to the various.

This is the first book primarily about the satellite payload of satellite communications systems. It represents a unique combination of practical systems engineering and communications theory. It tells about the satellites in geostationary and low-earth orbits today, both the so-called bent-pipe payloads and the processing payloads.

Audio Books & Poetry Community Audio Computers, Technology and Science Music, Arts & Culture News & Public Affairs Non-English Audio Spirituality & Religion Librivox Free Audiobook Confessions of a Serial Philosopher Coup Critique Podcast Body Language: The Yogis of India and Nepal Accept The Mystery podcast_between-panels_ Alexander.

However, the Shuttle Reference Manual includes plans for western test range satellite deployment missions from Vandenberg Air Force Base in California. Background and Status A high-level chronological overview of program milestones from to   This Interface Specification (IFS) identifies, defines, and controls the interface between the Reusable Reentry Satellite (RRS) Vehicle (RRV) Experiment Module (EM) and the Support Module (SM) equipment.

Contained in this specification are the physical, functional, and environmental interface requirements for the SM and EM.

Falcon 9 Launch Vehicle Payload User’s Guide stages are reusable, making them the world's first fully reusable launch vehicles. Payload customers using the Falcon 9 can take advantage of. The U.S. Air Force also conducted studies on semi-reusable spacecraft in the s.

NASA began work on an Integrated Launch and Re-entry Vehicle (ILRV) in. Next generation launchers ( future X-Pathfinder), reusable launch vehicles (RLV), Aerospace Vehicle Systems, Technology, Payload Launch Simulation, Aerospace Autonomous Operations, System studies for future space transport architectures, Rocket propulsion simulation, Space materials and structures, Aerothermodynamics, launcher health.

Atmospheric entry is the movement of an object from outer space into and through the gases of an atmosphere of a planet, dwarf planet, or natural are two main types of atmospheric entry: uncontrolled entry, such as the entry of astronomical objects, space debris, or bolides; and controlled entry (or reentry) of a spacecraft capable of being navigated or following a.

ISS Utilization: SIMPL (Satlet Initial-Mission Proofs and Lessons) / Kaber (NanoRacks Microsat Deployer) Spacecraft Kaber Launch Mission Status Satlet Technologies References. SIMPL is a microsatellite of NanoRacks, it is a modular satellite known as HISat (Hyper-Integrated Satellite) designed to provide complete satellite functionality in a nanosatellite scale.

Rocket Lab is redefining how we access space. Introducing Electron, Rocket Lab's latest launch vehicle - delivering small satellites to low Earth orbit at an unprecedented frequency.Get this from a library!

Experiment module/support module interface specification for the reusable reentry satellite. [Science Applications International Corporation.; Lyndon B. Johnson Space Center.;]. 1. INTRODUCTION A launch vehicle is used to carry a payload from the Earth's surface into outer space.

Usually the payload is an artificial satellite placed into the orbit of planets. Launch vehicles can be categorized into two: Expendable launch vehicles and Reusable launch vehicles. Expendable launch vehicles are designed for one-time use.