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  • 1
    Publication Date: 2019-09-01
    Print ISSN: 0094-5765
    Electronic ISSN: 1879-2030
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Published by Elsevier
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  • 2
    Publication Date: 2019-07-20
    Description: No abstract available
    Keywords: Lunar and Planetary Science and Exploration
    Type: M18-7125 , American Geophysical Union Fall Meeting (AGU 2018); Dec 10, 2018 - Dec 14, 2018; Washington, DC; United States
    Format: text
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  • 3
    Publication Date: 2019-07-13
    Description: No abstract available
    Keywords: Spacecraft Design, Testing and Performance
    Type: M19-7301 , The Space Astrophysics Landscape for the 2020s and Beyond; Apr 01, 2019 - Apr 03, 2019; Potomac, MD; United States
    Format: application/pdf
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  • 4
    Publication Date: 2019-07-13
    Description: No abstract available
    Keywords: Launch Vehicles and Launch Operations; Lunar and Planetary Science and Exploration
    Type: M18-6821 , Committee on Space Research (COSPAR) of the International Council of Scientific Unions Scientific Assembly (COSPAR 2018); Jul 14, 2018 - Jul 22, 2018; Pasadena, CA; United States
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  • 5
    Publication Date: 2019-12-03
    Description: Nearing its first launch, the Space Launch System (SLS), NASAs new super heavy-lift launch vehicle, offers highly energetic launches that deliver more mass and provide more volume in 8.4 m-diameter and potentially larger fairings to make a new generation of deep space missions possible. An evolvable launcher available in crew, crew with a co-manifested payload (CPL) and cargo-only configurations, SLS is a crucial capability to enable astronauts to return to the Moon, but it also offers key benefits for science missions. NASAs 21st-century return to the Moon recently received a formal name: the Artemis program. In addition to the core enabling capabilities of SLS and the Orion crew spacecraft, NASA will also enlist international and commercial partnerships for Artemis. The Agency intends to build a scientific outpost in lunar orbit, the Gateway, from which human and robotic missions to and from the surface can rendezvous. SLS will launch Orion on a series of missions leading to landing the first woman and the next man on the Moon as part of Artemis. SLS uses proven propulsion systems: two solid rocket boosters and four RS-25s engines that have been upgraded to provide more thrust and operate in the SLS environment. SLS Block 1 uses a modified Delta IV Heavy upper stage, called the Interim Cryogenic Propulsion Stage (ICPS) and lifts at least 26 metric tons (t) to trans-lunar injection (TLI). The Block 1 vehicle can also be outfitted with a 5 m-diameter fairing. Block 1B, the next major variant, also uses solid rocket boosters and RS-25 engines to achieve Earth escape velocity, but replaces the single-engine liquid hydrogen (LH2)/liquid oxygen (LOX) ICPS with a four-engine LH2/LOX Exploration Upper Stage (EUS) to increase mass to TLI to 34-37 t, depending on crew or cargo configuration. In the Block 1B crew configuration, a 10 m-tall Universal Stage Adapter (USA) connects the vehicle to Orion and can carry a CPL up to 10 t. The USA provides 286 m3 of unpressurized volume for payloads. For large payloads, 8.4 m- and 10 m-diameter cargo fairings in 19.1 m and 27.4 m lengths are possible. The ultimate SLS vehicle, Block 2, incorporates evolved boosters to reach a lift capacity of more than 45 t to TLI. The capabilities of SLS not only make new missions to the Moon possible, but also game-changing science missions, such as deployment of large-aperture space telescopes, spacecraft to the ice giants or even probes to the interstellar medium. This paper will discuss the capabilities of SLS, the vehicles planned evolution, missions that can effectively utilize the vehicle and manufacturing status of the vehicle.
    Keywords: Space Transportation and Safety
    Type: M19-7685 , International Astronautical Congress (IAC); Oct 21, 2019 - Oct 25, 2019; Washington, D.C.; United States
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  • 6
    Publication Date: 2019-07-13
    Description: Solar sail propulsion systems enable a wide range of missions that require constant thrust or high delta-V over long mission times. One particularly challenging mission type is a comet rendezvous mission. This paper presents optimal low-thrust trajectory designs for a range of sailcraft performance metrics and mission transit times that enables a comet rendezvous mission. These optimal trajectory results provide a trade space which can be parameterized in terms of mission duration and sailcraft performance parameters such that a design space for a small satellite comet chaser mission is identified. These results show that a feasible space exists for a small satellite to perform a comet chaser mission in a reasonable mission time.
    Keywords: Astrophysics
    Type: AAS/AIAA Space Flight Mechanics Conference; Jan 27, 2008 - Jan 31, 2008; Galveston, TX; United States
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  • 7
    Publication Date: 2019-07-13
    Description: Solar sail propulsion systems enable a wide range of space missions that are not feasible with current propulsion technology. Hardware concepts and analytical methods have matured through ground development to the point that a flight validation mission is now realizable. Much attention has been given to modeling the structural dynamics of the constituent elements, but to date an integrated system level dynamics analysis has been lacking. Using a multi-body dynamics and control analysis tool called TREETOPS, the coupled dynamics of the sailcraft bus, sail membranes, flexible booms, and control system sensors and actuators of a representative solar sail spacecraft are investigated to assess system level dynamics and control issues. With this tool, scaling issues and parametric trade studies can be performed to study achievable performance, control authority requirements, and control/structure interaction assessments.
    Keywords: Spacecraft Design, Testing and Performance
    Type: 2005 Joint Army Navy Nasa Air Force (JANNAF) Spacecraft Propulsion Subcommittee Joint Meeting; Dec 05, 2005 - Dec 08, 2005; Monterey, CA; United States
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  • 8
    Publication Date: 2019-09-07
    Description: No abstract available
    Keywords: Launch Vehicles and Launch Operations
    Type: M19-7607 , AIAA Propulsion and Energy Forum; Aug 19, 2019 - Aug 22, 2019; Indianapolis, IN; United States
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  • 9
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    In:  CASI
    Publication Date: 2019-12-04
    Description: No abstract available
    Keywords: Launch Vehicles and Launch Operations
    Type: M19-7707 , Interstellar Probe Workshop; Oct 16, 2019 - Oct 17, 2019; New York, NY; United States
    Format: application/pdf
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