• Publications
  • Influence
Rapid accommodation of payloads on the Standard Interface Vehicle through use of a standard payload interface
The STPSat-3 mission is the second flight of the Space Test Program Standard Interface Vehicle (STP-SIV) spacecraft platform. STP-SIV is a small spacecraft bus with well-defined, documented, andExpand
An overview of formation flying technology development for the Terrestrial Planet Finder mission
The objective of the Terrestrial Planet Finder (TPF) mission is to find and characterize earth-like planets orbiting other stars. Three architectural options are under consideration for this mission:Expand
Emirates Mars Mission (EMM) 2020 Overview
The United Arab Emirates (UAE) has entered the space exploration race with the announcement of the Emirates Mars Mission (EMM), the first Emirati mission to another planet, in 2014. Through thisExpand
Emirates Mars Mission (EMM) Overview
O. Sharaf, S. Amiri, S. AlMheiri, M. Wali, Z. AlShamsi, A. AlRais, I. AlQasim, K. AlHarmoodi, N. AlTeneiji, H. Almatroushi, Me. AlShamsi, Ma. AlShamsi, E. AlTeneiji, A. AlJanaahi, Mohammed Bin RashidExpand
Trajectory Design From GTO To Lunar Equatorial Orbit For The Dark Ages Radio Explorer (DARE) Spacecraft
The trajectory design for the Dark Ages Radio Explorer (DARE) mission con-cept involves launching the DARE spacecraft into a geosynchronous transfer orbit (GTO) as a secondary payload. From GTO, theExpand
Formation flying activities and capabilities at ball aerospace
1
Trajectory Design from GTO to Near-Equatorial Lunar Orbit for the Dark Ages Radio Explorer (DARE) Spacecraft
The trajectory design for the Dark Ages Radio Explorer (DARE) mission concept involves launching the DARE spacecraft into a geosynchronous transfer orbit (GTO) as a secondary payload. From GTO, theExpand