PPT-Integrating Payload Data Interfaces with LADEE Flight and G

Douglas Forman Millennium Engineering and Integration Company MEI LADEE FSW Payload IF Developer NASAAmes Research Center Moffett Field CA Craig Pires LADEE CampDH Lead NASA Matthew . Competition. Belhaj. , Y., Grant, A., . Rustan. , S. ., Sandler, M., . Guerr. , A.. Dr. . David . Cartes. . and Dr. Victor . DeBrunner. Design a canister satellite to protect a sensor payload. Must weigh 700 g with a tolerance of 10 g. 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. MnSGC. ). and . University of . Minnesota – Twin Cities. “Group 2”. Payload (mission name TBA). Conceptual Design Review – Dec. 1, 2010. U of . MN student . t. eam . m. embers . Kyle . Marek-Spartz. (kevinramus@vandals.uidaho.edu. ),. . K. Baird, C. Gonzalez, G. Wilson, W. . Taresh. , R. Riggs, G. . Korbel. , D. Atkinson, and the Idaho Near Space Engineering Team. University . of . Idaho. Abstract. . Chris . Rowan | Anthony Thompson | Philip . de la . Vergne. | Aaron . Wascom. | Brandon . Sciortino. http://. www.scienceclarified.com/Di-El/Electric-Arc.html. 1. Mission Goal. The goal of this payload is to understand the relationship of temperature and humidity on electric breakdown voltage.. 2013 High Altitude Balloon Design Program. MSGC BOREALIS Flight on 7/23/13. Program Overview. . 2. Left to Right: Katie, Mary, Allison, Genevieve, Tesha and Kasandra. Payload Prep (7/23/13 – 7:22am). Payload Design Project. Critical Design Review . July 17, 2012. Design Team:. . Jen Hoff (EE. ). Kate Ferris (EE. ). Alison . Figueira. (CS). . Makenzie. . Guyer. (CS). . Kaysha. Young (ME/MET). Mission Operations. Nathaniel Benz . Millennium Integration and Engineering Co.. . Lunar Atmosphere and Dust Environment Explorer (LADEE) was a NASA mission that will orbited the Moon and its main objective is to characterize the atmosphere and lunar dust environment. . Goal Statement. Objective: Design, develop, launch and retrieve a scientific payload which exceeds 100,000 . ft. in altitude. Payload must measure T and P throughout the entire flight, and must return video and photographic evidence covering the flight duration. . Tully . Baetz. Raymond Dao. Caleb . Ogg. 1. Mission Statement. The . DemoSat. . Project shall test several components of . the ALL-STAR mission in order to reduce risks in those areas. . Mission Objectives. Updates. USIP launches asap. HASP- waiting for ozone sensor. LMAH V habitat launch. Pre- flight roles. Flight prediction. Weather. File NOTAM. Heavy supplies/state vehicles. Payloads. Weights. Tracking and cameras. CSBF ICD for USIP Potential Payloads USIP Introduction CSBF provides space on a dedicated CSBF test flight for additional USIP funded payloads. Generally speaking, since configurations can change based on CSBF test articles, the Gondola utilized has 6 available spaces. 4 30”X30” Gondola Top spaces, and 2 40”X30”X28” spaces on the middle shelf. Flight requirements generally dictate a launch at 7am, 2 hours ascent to 115Kft, and a minimum of 2 hours at float. Harding . University Flying Bison 2010 USLI Team. Team Official. Project Progress Manager. Safety Officer. Edmond Wilson. Cortney, Mgr.. Edmond Wilson. Airframe. Motor. Science Payload. Avionics. Launch Operations. Contact: Irina Trefilova. E-mail:info@unmanned.ru. Tel.:+7(3412)51-51-65. 1. www.unmanned.ru. 2. 2. License for geodetic and mapping . services on the federal level. License . for aircrafts design, .