PPT-Estimating Flight Software Risk for a Space Launch Vehicle

2014 RAMS VII Workshop November 4 2014 S Novack 1 SHatfield 1 M Al Hassan 1 JBales 2 P Britton 2 FHark 1 JStott 2 1 Bastion Technologies Inc 2 NASA Marshall Space Flight Center. IntimiGATOR. . FRR. Outline. Overview. System Design. Recovery Design. Payload Design. Simulations and Performance. Testing . Project Summary . Launch Vehicle. The launch vehicle is designed to reach an altitude of a mile. 50. th. AIAA-JPC Conference, July 29, 2014. Cleveland, OH. All m. embers: . Space Propulsion Synergy Team . – http:spacepropulsion.us. Douglas . G. Thorpe, Co-Founder: http://theUSAparty.com. Russel. Cardiopulmonary . problems. . (heart. , lungs). . The body has evolved to spend 2/3rds of its time upright within a 1g vertical field. The result of microgravity is to disturb this. The obvious change is in the fluid distribution, with a general shift to the torso and head. . Reaction Wheel. How it creates Propulsion. Reaction wheels actually do NOT create propulsion, they only create rotation.. Main components of the system. Electric motor. Flywheel. When would it be most effective?. Rachael . E. . Tompa. Stanford Intelligent Systems Laboratory. Motivation. 2. Problem: . L. aunch vehicle anomaly can lead to 10,000+ . pieces of . debris . P. rojected . increase in commercial space . 50. th. AIAA-JPC Conference, July 29, 2014. Cleveland, OH. All members: . Space Propulsion Synergy Team . – . http:spacepropulsion.org. Douglas G. Thorpe, Co-Founder: http://theUSAparty.com. Russel. Engineering . Sheldon Clark. Raytheon. Agenda. Today’s Activities:. Overview of Aerospace Engineering. What is a satellite?. Introduction to our mission. Satellite Subsystem overview. Final design preparation. Presented to the Review of U.S. Human Spaceflight Plans Committee . June 17, 2009. 1. 1990’s NASA sponsored Shuttle C. Side-Mount Shuttle Derived Vehicle Concepts. Have Matured Via Several Major Design Studies. Christopher Krupiarz. Christopher.Krupiarz@. jhuapl.edu. Solar Probe Plus. . A NASA Mission to Touch the Sun. Overarching Science Objective. To determine the structure and dynamics of the Sun’s coronal magnetic field, understand how the solar corona and wind are heated and accelerated, and determine what mechanisms accelerate and transport energetic particles. . Vehicle dimensions, materials, and justifications. Static stability margin. Plan for vehicle safety verification and testing. Baseline motor selection and justification. Thrust-to-weight ratio and rail exit velocity. FEDERAL AVIATION ADMINISTRATIONORDER 88002National PolicyEffective date 07/20/2021SUBJFAA Commercial Space Astronaut Wings Program1Purpose of This Order This Order provides guidelines eligibility and AE 4361HOURS3-0-3CATALOG DESCRIPTIONThis course introduces the foundations and analysis of space flight operations for human and robotic space missionsPREREQUISITESAE 3330Introduction to Aerospace Veh Bhavya Lal PhD Research Staff Member Emily Nightingale Science Policy Fellow Science and Technology Policy Institute 1899 Pennsylvania Avenue NW Washington DC 20006 Abstract Despite decades of debat 2017 ICEAA Professional Development . & Training Workshop. James R. Black. June 2017. 1. Bio. Presenter: James “Jay” Black has 13 years of cost estimating experience and currently works as a software project manager for the Administration...