Design, development, and flight of the NEAR propulsion system

Johns Hopkins APL Technical Digest (Applied Physics Laboratory)

Volumn 19, Issue 2, 1998, Pages 174-184

  Mosher, Larry E ^{a,b,c,d,e,f,g,h}   Wiley, Sam ^h,i,j,k  

^a Cayuga Community College   (United States)

^b MICHIGAN STATE UNIVERSITY   (United States)

^c DREXEL UNIVERSITY   (United States)

^d Martin   (United States)

^e Bell Aerospace   (United States)

^f Fairchild Space Company   (United States)

^g APL   (United States)

^h NEAR Propulsion System

ⁱ CALIFORNIA STATE UNIVERSITY   (United States)

^j AEROJET ROCKETDYNE   (United States)

^k ALAS LEAP X Propulsion System

more..

Author keywords

Bipropellant; NEAR propulsion system; Regulated pressurization

Indexed keywords

ANTENNAS; INTERPLANETARY SPACECRAFT; SOLAR CELL ARRAYS; SPACE FLIGHT; SPACE RENDEZVOUS; TRAJECTORIES;

NEAR EARTH ASTEROID RENDEZVOUS (NEAR) SPACECRAFT;

SPACECRAFT PROPULSION;

EID: 0032048799     PISSN: 02705214     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (3)

1. Near Earth Asteroid Rendezvous (NEAR) Propulsion System Interface Control Document (ICD), The Johns Hopkins University Applied Physics Laboratory, Laurel, MD (May 1995).
2. Thunker, R. R., Eastern Range Regulation 127-1 Tailored for the Near Earth Asteroid Rendezvous (NEAR) Payload, U.S. Air Force (30 June 1993, Revised Dec 1994).
3. Standard General Requirements for Safe Design and Operation of Pressurized Missile and Space Systems, MIL-STD-1522A, U.S. Air Force (28 May 1984).