IGNITON AND COMBUSTION CHARACTERISTICS OF METALLIZED PROPELLANTS - PHASE II
- Author(s):
- Mueller, D.C. ( The Pennsylvania State University )
- Turns, S.R.
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1994
- Issue:
- NASA-CR-195197
- No.:
- G3/28 0204165
- Pt.:
- NAS 1.26:195197
- Paper no.:
- N94-24700
- Page(from):
- 1
- Page(to):
- 27
- Pages:
- 27
- Pub. info.:
- National Aeronautics and Space Adminstration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
National Aeronautics and Space Adminstration |
Society of Automotive Engineers |
National Aeronautics and Space Adminstration |
8
Technical Paper
Combustion and Performance Characteristics of a DI Diesel Engine Operating from Low to High Natural Gas Supplement Ratios at Various Operating Conditions.
Society of Automotive Engineers |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Early Direct-Injection, Low-Temperature Combustion of Diesel Fuel in an Optical Engine Utilizing a 15-Hole, Dual-Row, Narrow-Included-Angle Nozzle.
Society of Automotive Engineers |