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Volumn , Issue , 1999, Pages

Performance and life testing of small han thrusters

Author keywords

[No Author keywords available]

Indexed keywords

AMINO ACIDS; COMBUSTION; ELECTRON EMISSION; EXHAUST GASES; METALS; MONOPROPELLANTS; PRECIOUS METALS; PROPULSION; ROCKET ENGINES; ROCKETS;

EID: 84963850013     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (14)

References (17)
  • 1
    • 84963902110 scopus 로고    scopus 로고
    • This work is being performed under NASA contract NAS3-27782 from the NASA Glenn Research Center
    • This work is being performed under NASA contract NAS3-27782 from the NASA Glenn Research Center.
  • 2
    • 84963902118 scopus 로고    scopus 로고
    • (NASA GRC), HAN Based Monopropellant Assessment for Spacecraft, AIAA Paper 96-2863
    • Jankovsky, R.S. (NASA GRC), HAN Based Monopropellant Assessment for Spacecraft, AIAA Paper 96-2863.
    • Jankovsky, R.S.1
  • 7
    • 84963883883 scopus 로고    scopus 로고
    • Non-toxic Orbital 5 Maneuvering and Reaction Control Systems for Reusable Spacecraft. El. Discussions with K. Mahaffy (AFRL), August
    • Hurlbert, E., Appleshitge, Nguyen, Reed, Baojiong, Yue, Non-toxic Orbital 5 Maneuvering and Reaction Control Systems for Reusable Spacecraft. El. Discussions with K. Mahaffy (AFRL), August 1997.
    • (1997) Appleshitge, Nguyen, Reed, Baojiong, Yue
    • Hurlbert, E.1
  • 8
    • 84963883852 scopus 로고    scopus 로고
    • PL-TR-96-3006, Hybrid Propulsion for Air Force Missions Study, March
    • PL-TR-96-3006, Hybrid Propulsion for Air Force Missions Study, March 1997.
    • (1997)
  • 9
    • 84963890909 scopus 로고
    • U.S. Patent 4, 527, 389, Highly Soluble, Non Hazardous Hydroxylammonium Salt Solutions for Use in Hybrid Rocket Motors, July
    • U.S. Patent 4, 527, 389, Highly Soluble, Non Hazardous Hydroxylammonium Salt Solutions for Use in Hybrid Rocket Motors, July 1985.
    • (1985)
  • 10
    • 84963919590 scopus 로고    scopus 로고
    • U.S. Patent 5, 485, 722, January 23, Catalytic Decomposition of Hydroxylammonium Nitrate Based Monopropellants
    • U.S. Patent 5, 485, 722, January 23, 1996, Catalytic Decomposition of Hydroxylammonium Nitrate Based Monopropellants.
    • (1996)
  • 11
    • 84963890904 scopus 로고    scopus 로고
    • Work performed at PAC under contract F33-93- C-2360 from AFRL
    • Work performed at PAC under contract F33-93- C-2360 from AFRL.
  • 12
    • 84963843470 scopus 로고    scopus 로고
    • Investigation of Propulsion System Requirements for Spartan Lite, 12th Annual Conference on Small Satellites, SSC98-VIII-5
    • Urban, Gruner, Morrissey, and Sneiderman, Investigation of Propulsion System Requirements for Spartan Lite, 12th Annual Conference on Small Satellites, SSC98-VIII-5.
  • 13
    • 84963820433 scopus 로고    scopus 로고
    • Formulation of HAN-Based Monopropellants for Thruster Applications, JANNAF PDCS/S&EPS Joint Meeting, April
    • Wucherer, Christofferson, Meinhardt, Formulation of HAN-Based Monopropellants for Thruster Applications, JANNAF PDCS/S&EPS Joint Meeting, April 1999.
    • (1999)
  • 14
    • 84963803544 scopus 로고
    • AFRPL-TR-69-242, Hydrazine Nitrate Catalyst Development, Shell Development Company, August
    • AFRPL-TR-69-242, Hydrazine Nitrate Catalyst Development, Shell Development Company, August 1969.
    • (1969)
  • 15
    • 84963890897 scopus 로고
    • RRC 66-R-76, Design and Scaling Criteria For Monopropellant Hydrazine Reactors Employing Shell 405 Spontaneous Catalyst, January
    • RRC 66-R-76, Design and Scaling Criteria For Monopropellant Hydrazine Reactors Employing Shell 405 Spontaneous Catalyst, January 1967.
    • (1967)
  • 16
    • 84963883840 scopus 로고
    • AFRPL TR-77-6, Design and Scaling Manual for Long Life Monopropellant Engines, February
    • AFRPL TR-77-6, Design and Scaling Manual for Long Life Monopropellant Engines, February 1977.
    • (1977)
  • 17
    • 84963820436 scopus 로고
    • 67-P-302-1 A, Thrust Chamber Assembly, Monopropellant Performance Analysis, September
    • A 67-P-302-1 A, Thrust Chamber Assembly, Monopropellant Performance Analysis, September 1967.
    • (1967)


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.