Browsing JPL TRS 1992+ by Title

Now showing items 36303-36322 of 36386

The X/Ka-band Extragalactic Reference Frame

Garcia-Miro, Cristina; Sotuela, I.; Jacobs, C. S.; Clark, J. E.; Romero-Wolf, A.; Horiuchi, S.; Snedeker, L .G. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2012., 2012-03-05)
X/Ka-band feed for the DSN array

Gatti, Mark; Imbriale, William; Hoppe, Daniel; Reilly, Harry; Prater, Jack; Britcliffe, Michael (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2003., 2003-12)
X/Ka-band one-meter deployable mesh reflector for Deep Space Network telecommunication

Chahat, Nacer; Sauder, Jonathan; Mitchell, Matthew; Beidleman, Neal; Freebury, Gregg (Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2019, 2019-03-31)

A deployable one meter mesh reflector compatible with 12U-class CubeSat is introduced for telecommunication. It is compatible with NASA’s deep-space network (DSN) at X-band (i.e., uplink: 7.145-7.19 GHz; downlink: 8.4-8.45 ...
X/X/Ka-Band Horn Design

Chen, Jacquline; Stanton, Philip H.; Reilly, Harry F. (1996-07-21)

Tne NASA's Deep Space Network has a need for a multi frequency horn for simultaneous X/X/Ka-band operation in a beam waveguide antenna. The multi frequency horn will receive X-band downlink (8.4-8.5 GHz) and Ka-band ...
X2000 advanced avionics characterization study

Day, L.; Meyer, D.; Nicolich, N.; Steele, R.; Uchenik, I.; Vines, K. (2003-03-08)

The characterization study has shown that adjustments in an application's data accesses can easily create a performance difference of three or more times in actual applications. In general, by iterating over a small portion ...
X2000 advanced avionics characterization study : Living in the modern world of difficult to predict processor performance.

Day, L. E.; Meyer, D.; Nicolich, N.; Steele, R.; Uchenik, I.; Vines, K. (2002-11-19)

The characterization study has shown that adjustments in an application's data accesses can easily create a performance difference of three or more times in actual applications. In general, by iterating over a small portion ...
X2000 advanced avionics development

Blue, R. C.; Thomas, V. (2002-02-13)
X2000 Advanced Avionics Project development of a new generation of avionics for space applications

Blue, R. C.; Bolotin, G. S. (2003-03-08)

This paper will describe the system architecture, the avionics components, the key performance and reliability requirements, and the current development status of the X2000 Avionics.
X2000 advanced avionics project performance characterization study

Day, L.; Meyer, D.; Nicolich, N.; Steele, R.; Uchenik, I.; Vines, K. (2002-08-07)
X2000 advanced avionics project, development of a new generation of avionics for space application

Blue, R.; Bolotin, G. (2003-03-08)
X2000 Briefing - Introduction

Clark, K. B. (2002-02-13)
X2000 command and data handling system development

Arakai, G.; Geer, D. A.; Strauss, K.; Kaczinski, C.; Day, L.; Theberge, B. (2002-02-13)
X2000 Flight Missions Utilizing Common Modular Components

Smyth, David E.; Price, Humphrey W. (1998-03-21)

A software and hardware architecture was developed for the X2000 bus that is modular, scaleable, and upgradable. It will enable the procurement of highly capable, low mass flight systems that can perform the mission set ...
X2000 Power System Architecture

Franco, Lauro A. (1997-08-01)

JPL is starting a new program that targets the exploration of the outer planets in our Solar System. The Advanced Deep Space System Development Program (ADSSDP) is to provdie a spacecraft system for a series of missions ...
X2000 power system control architecture

Carr, Greg; Wester, Gene; Ruiz, B. Ian; Burke, Gary R.; Lung, Gerald; Whitaker, William D. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2005, 2005-04)
X2000 power system electronics development

Carr, Greg; Deligiannis, Frank; Franco, Lauro; Jones, Loren; Lam, Barbara; Nelson, Ron; Pantaleon, Jose; Ruiz, Ian; Treichler, John; Wester, Gene; Sauers, Jim; Giampoli, Paul; Haskell, Russ; Mulvey, Jim; Repp, John (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2005., 2005-08)

The X2000 Power System Electronics (PSE) is a Jet Propulsion Laboratory (JPL) task to develop a new generation of power system building blocks for potential use on future deep space missions. The effort includes the ...
X2000 power system electronics development

Carr, G. A. (2002-03-09)

The Europa Orbiter mission, currently baselined for launch in March 2008, is intended to follow up on tantalizing results from the Gulileo spacecraft, data from which suggests that there may be a global Ocean underneath ...
X2000 Power System Electronics Development

Carr, G.; Wester, G.; Sauers, J.; Danielak, B.; Holic, J.; Hogue, D. (2000-03-18)

The Deep Space System Technology (DSST) Program (X2000) is managed by JPL for NASA.
The X2000 Program

Deutsch, L. (1998-12)
The X2000 Program - An Institutional Approach to Enabling Smaller Spacecraft

Deutsch, L.; Salvo, C.; Woerner, D. (1999-04-12)

Now showing items 36303-36322 of 36386

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