Blank Cover Image

A LIFE TEST OF A 22-NEWTON (5-lbf) HYDRAZINE ROCKET

Author(s):
Meng, P. R. et al. ( NASA )  
Publication title:
NASA Technical Reports(N88-)
Pub. Year:
1987
Issue:
NASA-TM-100232
No.:
G3/20 0107554
Pt.:
NAS1.15:100232
Paper no.:
N88-11750
Page(from):
1
Page(to):
12
Pages:
12
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

Similar Items:

1 Technical Paper Demonstration Testing of a Long-Life 5-Lbf (22-N) MR-106L Monopropellant Hydrazine Rocket Engine Assembly

Wilson, M.

American Institute of Aeronautics and Astronautics
7 Technical Paper RIT-22 Ion Propulsion System: 5000h Endurance Test Results and Life Prediction

H. Leiter, R. Kukies, R. Killinger, L. Bonelli, S. Scaranzin, F. Scortecci, H. Neumann, M. Tartz

American Institute of Aeronautics and Astronautics
2 Technical Paper Delta-Qualification of a 22N (5.0 lbf) MR-106B Monopropellant Hydrazine Thruster for the Mars Odyssey Spacecraft

Morgan,Olwen M., Fischer,Timothy L., Guernsey,Carl S.

American Institute of Aeronautics and Astronautics
8 Technical Paper Extreme temperature operation of a hydrazine rocket engine

Reitan, Thane D., Durbin, Mike R.

American Institute of Aeronautics and Astronautics
3 Technical Paper Demonstration Tests Results for 1 Lbf Long Life Monopropellant Thruster

J. Gervasi, M. Marvin, K. Josten, H. Conomos, R. Driscoll

American Institute of Aeronautics and Astronautics
9 Technical Paper Test of a Turbo-Pump Fed Miniature Rocket Engine

C. Scharlemann, M. Schiebl, K. Marhold, M. Tajmar, P. Miotti, C. Guraya, F. Seco, C. Kappenstein, Y. Batonneau, R. …

American Institute of Aeronautics and Astronautics
4 Technical Paper Transient thermal modelling of ARC 5 lbf Bi-propellant thruster

Purohit, G.P., Donatelli, P.A., Dhir, V.K., Driscoll, R.J.

American Institute of Aeronautics and Astronautics
10 Technical Paper Off-Limit Testing of the Model R-4D 110 LBF (490 N) Bipropellant Rocket Engine

Stechman, C., Krismer, D., Ueno, F.

American Institute of Aeronautics and Astronautics
5 Technical Paper RIT-22 Ion Engine Development - Endurance Test and Life Prediction

H. Leiter, R. Kukies, R. Killinger, E. Bonelli, S. Scaranzin, F. Scortecci

American Institute of Aeronautics and Astronautics
11 Technical Paper The performance characterization of a small hybrid motor for solid rocket motor material testing

Letson, M., Peralta, P., Bunker, R.

American Institute of Aeronautics and Astronautics
6 Technical Paper Upcoming improvements to the gas turbine performance test code PTC 22

Allen, R. P.

The American Society of Mechanical Engineers
12 Technical Paper Intermediate Temperature Fluids Life Tests - Experiments

W. Anderson, R. Bonner, P. Dussinger, J. Hartenstine, D. Sarraf, I. Locci

American Institute of Aeronautics and Astronautics
1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12