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astronautix.com Alphabetic Index - N
N Block V - Rocket Stage - Russia - Lox/Kerosene - 150,000 kg - See N3 Block A
N-11 1963 - V - Rocket Stage - Russia - Lox/Kerosene - 70,000 kg
N-11 1963 - Launch Vehicle - Russia
N-11 Block A - Rocket Stage - Russia - Lox/Kerosene - 485,000 kg
N-11 Block B - Rocket Stage - Russia - Lox/Kerosene - 192,000 kg
N-111 - A - Rocket Stage - Russia - Lox/Kerosene - 192,000 kg
N-111 - Launch Vehicle - Russia
N-11GR - V - Rocket Stage - Russia - Lox/Kerosene - 8,200 kg
N-11GR - Launch Vehicle - Russia
N-1 - Launch Vehicle - Russia - See N1 1964
N-2 - Launch Vehicle - Japan
N-4 - Spacecraft - Astronomy - Cosmic Ray - USSR
N-6 - Spacecraft - Astronomy - Cosmic Ray - USSR
N-IF 1965 - Launch Vehicle - Russia
N-IFV-II, III - Launch Vehicle - Russia
N-IFV-III - Launch Vehicle - Russia
N-IM 1965 - Launch Vehicle - Russia
N-IMV-II, III - Launch Vehicle - Russia
N-IMV-III - Launch Vehicle - Russia
N-IU - Launch Vehicle - Russia
N-IUV-III - Launch Vehicle - Russia
N-STAR - Space Project - Communications -
N1 1962 - A - Rocket Stage - Russia - Lox/Kerosene - 1,384,000 kg
N1 1962 - B - Rocket Stage - Russia - Lox/Kerosene - 506,000 kg
N1 1962 - V - Rocket Stage - Russia - Lox/Kerosene - 193,000 kg
N1 1962 - Launch Vehicle - Russia
N1 1964 - A - Rocket Stage - Russia - Lox/Kerosene - 1,942,000 kg
N1 1964 - B - Rocket Stage - Russia - Lox/Kerosene - 506,000 kg
N1 1964 - V - Rocket Stage - Russia - Lox/Kerosene - 193,000 kg
N1 1964 - Launch Vehicle - Russia
N1 Block A - Rocket Stage - Russia - Lox/Kerosene - 1,880,000 kg
N1 Block B - Rocket Stage - Russia - Lox/Kerosene - 560,700 kg
N1 Block D - Rocket Stage - Russia - Lox/Kerosene - 18,200 kg
N1 Block G - Rocket Stage - Russia - Lox/Kerosene - 61,800 kg
N1 Block R - Rocket Stage - Russia - Lox/LH2 - 23,000 kg
N1 Block Sr - Rocket Stage - Russia - Lox/LH2 - 77,900 kg
N1 Block S - Rocket Stage - Russia - Lox/LH2 - 58,000 kg
N1 Block V-III - Rocket Stage - Russia - Lox/LH2 - 325,000 kg
N1 Block V-II - Rocket Stage - Russia - Lox/LH2 - 805,000 kg
N1 Block V - Rocket Stage - Russia - Lox/Kerosene - 188,700 kg
N1 Nuclear AF - Launch Vehicle - Russian
N1 Nuclear AF - Rocket Stage - Russia - Nuclear/LH2 - 800,000 kg
N1 Nuclear A - Launch Vehicle - Russian
N1 Nuclear A - Rocket Stage - Russia - Nuclear/LH2 - 700,000 kg
N1 Nuclear V-Bioshield - Rocket Stage - Russia - Nuclear/LH2 - 2,000,000 kg
N1 Nuclear V-B - Launch Vehicle - Russian
N1 Nuclear V - Launch Vehicle - Russian
N1 Nuclear V - Rocket Stage - Russia - Nuclear/LH2 - 1,500,000 kg
N1-MOK - Launch Vehicle - Russia
N1-MOK - Rocket Stage - Russia - Air/Lox/LH2 - 1,200,000 kg
N11 - Launch Vehicle - Russia
N1 - Article: Completely updated! Part 2 of the story of the design, construction, and collapse of the immense N1 Soviet super booster.
N1F 1965 - A - Rocket Stage - Russia - Lox/Kerosene - 1,940,000 kg
N1F 1965 - B - Rocket Stage - Russia - Lox/Kerosene - 590,000 kg
N1F 1965 - V - Rocket Stage - Russia - Lox/Kerosene - 300,000 kg
N1F Block A - Rocket Stage - Russia - Lox/Kerosene - 2,070,000 kg
N1F Block B - Rocket Stage - Russia - Lox/Kerosene - 620,000 kg
N1F Block V - Rocket Stage - Russia - Lox/Kerosene - 210,000 kg
N1F Sr - Launch Vehicle - Russia
N1F-L3M - Launch Vehicle - Russia
N1F - Launch Vehicle - Russia
N1 - Launch Vehicle - Russia
N1M 1965 - A - Rocket Stage - Russia - Lox/Kerosene - 3,800,000 kg
N1M 1965 - B - Rocket Stage - Russia - Lox/Kerosene - 620,000 kg
N1M 1965 - V - Rocket Stage - Russia - Lox/Kerosene - 355,000 kg
N1M - Launch Vehicle - Russia
N1U 1965 - A - Rocket Stage - Russia - Lox/Kerosene - 1,934,000 kg
N1U 1965 - B - Rocket Stage - Russia - Lox/Kerosene - 506,000 kg
N1U 1965 - V - Rocket Stage - Russia - Lox/Kerosene - 193,000 kg
N3 Block A - Rocket Stage - Russia - Lox/Kerosene - 150,000 kg
Nadezhda - Spacecraft - Navigation - - USSR
Nagel - Steven Ray Nagel - American Astronaut - 1978 NASA Group
Nahuel - Space Project - Communications -
Nair - Paramaswaren Radhakrishnan Nair - Indian Astronaut - Payload Specialist
Nakov - Ivan Nakov - Cosmonaut candidate - 1978 Intercosmos Group (Candidate)
Nanosat SSTL - Spacecraft - Technology - - UK
Naryad - Spacecraft - Military- ASAT - USSR - See IS-MU
Narymurti - Bambang Narymurti - Astronaut candidate - Payload Specialist (Candidate)
NASA 747 - Rocket Stage - USA - Air/Kerosene - 276,364 kg
NASA ACRV - Spacecraft - - - USA
NASA Lifting Body - Space Project - Manned - Spaceplane
NASA Mark III - Spacecraft - Manned - Space Suits - USA
NASDA H-2 Transfer Vehicle - Spacecraft - - - Japan
NASDA Japanese Experiment Module - Spacecraft - - - Japan
Nash - J S Nash - American Test Pilot - Test Pilot (USAF)
NASP (National Aerospace Plane); Orient Express - Rocket Stage - USA - Air/Slush LH2 - 140,000 kg - See X-30
National Aerospace Plane - Launch Vehicle - USA - See X-30
National Launch System - Launch Vehicle - USA - See NLS HLV
National Launch System - Rocket Stage - USA - Lox/LH2 - 815,732 kg - See NLS Core
NATO 1 - Spacecraft - Communications - Military - UK
NATO 3 - Spacecraft - Communications - Military - NATO
NATO - Space Project - Communications - Military
Nauka-2 - Spacecraft - Earth - Magnetosphere - USSR
Nauka - Spacecraft - Earth - Magnetosphere - USSR
Navaho G-26 - Launch Vehicle - USA
Navaho G-38 - Launch Vehicle - USA
Navaho X-10 - Launch Vehicle - USA
Navaho X-10 - Rocket Stage - USA - Air/Kerosene - 19,183 kg
Navaho/X-15 - Launch Vehicle -
Navaho - Launch Vehicle Family
Navaho - Space Project - Manned - Spaceplane
Navstar - Space Project - Technology - Navigation
Navy SLV - Spacecraft - Manned - Lunar Lander - USA
Navy SLV - Space Project - -
NAZ-3 - Spacecraft - Manned - Space Suits - USSR
NB-52 - Rocket Stage - USA - Air/Kerosene - 177,273 kg
Near Earth Asteroid Rendezvous - Spacecraft - Planetary- Asteroid - United States - See NEAR
NEAR - Spacecraft - Planetary - Asteroid - United States
Nedelin - Article: James Oberg's classic account of the greatest disaster in space history.
Nelson Bill - Clarens William (Bill) Nelson - American Astronaut - Payload Specialist
Nelson - Dr George Driver (Pinky) Nelson - American Astronaut - 1978 NASA Group
Nelyubov - Grigori Grigoyevich Nelyubov - Russian Cosmonaut - 1960 Air Force Group
Neman - Spacecraft - Surveillance- Military - USSR - See Neman
Neri Vela - Rodolfo Neri Vela - Mexican Astronaut - Payload Specialist
Nerva - Rocket Stage - USA - Nuclear/LH2 - 178,321 kg
Nerva 12 GW - Rocket Engine - USA - Nuclear/LH2 propellants - kgf
NERVA 1mlbf - Rocket Engine - USA - Nuclear/LH2 propellants - 914,000 kgf
Nerva 2/NTR - Rocket Stage - USA - Nuclear/LH2 - 158,400 kg
Nerva 2 - Rocket Engine - USA - Nuclear/LH2 propellants - 88,451 kgf
Nerva 2 - Launch Vehicle - USA
Nerva NTR - Rocket Engine - USA - Nuclear/LH2 propellants - 34,000 kgf
NERVA/Lox Mixed Cycle - Rocket Engine - USA - Nuclear/Lox/LH2 propellants - 2,460,250 kgf
Nerva; Rover; Pluto - Rocket Stage - USA - Nuclear/LH2 - 178,321 kg - See Nerva
Nerva - Rocket Engine - USA - Nuclear/LH2 propellants - 27,206 kgf
Nerva - Launch Vehicle Family
NERVA - Space Project - Launch vehicle -
Nespoli - Paolo Alberto Nespoli - Italian Astronaut - 1998 ESA Group
Neubeck - Francis Gregory Neubeck - American Astronaut - 1965 USAF MOL Group 1
New Launch System - Launch Vehicle - USA - See NLS
Newman - Dr James (Jim) Hansen Newman - American Astronaut - 1990 NASA Group
Newton's Orbital Cannon - Launch Vehicle - UK
NEXT - Launch Vehicle - Israel - See Shavit 1
Nguyen - Nguyen Van Kock - Vietnamese Cosmonaut candidate - 1979 Intercosmos Group (Candidate)
Nicollier - Claude Nicollier - Swiss Astronaut - 1980 NASA Group
NII 612 kgf - Rocket Engine - Russia - N2O4/UDMH propellants - 612 kgf
Nika-T - Spacecraft - Materials - - Russia
Nike-Asp - Launch Vehicle - USA
Nike-Cajun - Launch Vehicle - USA
Nike-Deacon - Launch Vehicle - USA
Nike-Zeus - Launch Vehicle - USA
Nikitsky - Vladimir Prtrovich Nikitsky - Russian Cosmonaut candidate - 1966 Civilian Engineer Group (Candidate)
Nikolayev Oleg - Oleg Nikolaevich Nikolayev - Russian Cosmonaut candidate - 1965 Physician Group (Candidate)
Nikolayev Sergei - Sergei Olegovich Nikolayev - Russian Cosmonaut candidate - 1965 Physician Group (Candidate)
Nikolayev - Andrian Grigoryevich Nikolayev - Russian Cosmonaut - 1960 Air Force Group
Nilesat - Space Project - Communications -
Nimbus - Spacecraft - Earth - Weather - USA
NK-15 - Rocket Engine - Russia - Lox/Kerosene propellants - 157,400 kgf
NK-15F - Rocket Engine - Russia - Lox/Kerosene propellants - 222,300 kgf - See NK-15F
NK-15V - Rocket Engine - Russia - Lox/Kerosene propellants - 168,000 kgf
NK-15VM - Rocket Engine - Russia - Lox/LH2 propellants - 200,000 kgf - See NK-15VM
NK-19, NK-21 - Rocket Engine - Russia - Lox/Kerosene propellants - 45,000 kgf - See NK-9V
NK-19 - Rocket Engine - Russia - Lox/Kerosene propellants - kgf
NK-21 - Rocket Engine - Russia - Lox/Kerosene propellants - 45,785 kgf - See NK-9V-11D53
NK-231 - Rocket Engine - Russia - Air/Kerosene propellants - 23,100 kgf - See NK-231
NK-31 - Rocket Engine - Russia - Lox/Kerosene propellants - 41,000 kgf
NK-33 LH2 Mod + 4 x LACE - Rocket Engine - Russia - Air/Lox/LH2 propellants - 100,000 kgf
NK-33 LH2 Mod - Rocket Engine - Russia - Air/Lox/LH2 propellants - 100,000 kgf - See NK-33 LH2 Mod + 4 x LACE
NK-33 - Rocket Engine - Russia - Lox/Kerosene propellants - 167,000 kgf - See NK-33
NK-35 - Rocket Engine - Russia - Lox/LH2 propellants - 200,000 kgf
NK-39 - Rocket Engine - Russia - Lox/Kerosene propellants - 41,000 kgf
NK-43 - Rocket Engine - Russia - Lox/Kerosene propellants - 179,000 kgf - See NK-43
NK-9 - Rocket Engine - Russia - Lox/Kerosene propellants - 45,000 kgf
NK-9V-11D53 - Rocket Engine - Russia - Lox/Kerosene propellants - 45,785 kgf
NK-9V-11D54 - Rocket Engine - Russia - Lox/Kerosene propellants - 40,000 kgf
NK-9V - Rocket Engine - Russia - Lox/Kerosene propellants - kgf - See NK-21
NLS Core - Rocket Stage - USA - Lox/LH2 - 815,732 kg
NLS HLV - Launch Vehicle - USA
NLS HLV - Rocket Stage - USA - Lox/LH2 - 833,732 kg
NLS Semistage - Rocket Stage - USA - Lox/LH2 - 36,000 kg
NLS - Launch Vehicle - USA
N - Launch Vehicle Family
N - Launch Vehicle - Japan
Nodong - Rocket Engine - Korea North - Nitric acid/UDMH propellants - 14,718 kgf
Noguchi - Soichi Noguchi - Japanese Astronaut - 1996 NASDA Group
Nomad - Rocket Engine - - LF2/Hydrazine propellants - 5,450 kgf - See G-1
None - Rocket Engine - na - propellants - kgf
Nonweiler Waverider - Spacecraft - Manned - Spaceplane - UK
Noordung - Spacecraft - Manned - Space Station - USA
Nordsieck - Dr Kenneth Hugh Nordsieck - American Astronaut - Payload Specialist
Noriega - Carlos Ismael Noriega - American Astronaut - 1995 NASA Group
Norma - Launch Vehicle - Russia
North American - Spacecraft - Manned- Logistics - USA - See Apollo RM
Northrop LBEC - Spacecraft - Manned - Bailout - USA
Northrop Project 7969 - Spacecraft - Manned - Spacecraft - USA
Northrop sled 4000 Ibf thrust - Rocket Engine - USA - propellants - kgf
Nose-Cone-Test - Spacecraft - Technology - RV - USA
NOSS-2 subsatellite - Spacecraft - ELINT - Naval reconnaisance - USA
NOSS-2 - Spacecraft - ELINT - Naval reconnaisance - USA
NOSS-Subsat - Spacecraft - ELINT - Naval reconnaisance - USA
NOSS - Spacecraft - ELINT - Naval reconnaisance - USA
NOTS 100A - Rocket Engine - USA - Solid propellants - kgf
NOTS-1 - Rocket Engine - USA - Solid propellants - 5,441 kgf
NOTS-3 - Rocket Engine - USA - Solid propellants - 231 kgf
NOTS-4 - Rocket Engine - USA - Solid propellants - 72 kgf
NOTS - Launch Vehicle - USA
Nova 2 F-1 Module - Rocket Stage - USA - Lox/Kerosene - 1,134,000 kg
Nova 4 J-2 - Rocket Stage - USA - Lox/LH2 - 771,000 kg
Nova 4L - Launch Vehicle - USA
Nova 4S - Launch Vehicle - USA
Nova 59-4-1 - Rocket Stage - USA - Lox/Kerosene - 2,177,000 kg
Nova 59-4-2 - Rocket Stage - USA - Lox/Kerosene - 590,000 kg
Nova 59-4-3 - Rocket Stage - USA - Lox/LH2 - 168,000 kg
Nova 59-4-4 - Rocket Stage - USA - Lox/LH2 - 68,000 kg
Nova 5S - Launch Vehicle - USA
Nova 60-8-1 - Rocket Stage - USA - Lox/Kerosene - 3,628,000 kg
Nova 60-8-2 - Rocket Stage - USA - Lox/LH2 - 680,000 kg
Nova 60-8-3 - Rocket Stage - USA - Lox/LH2 - 227,000 kg
Nova 7S - Launch Vehicle - USA
Nova 8L Mod - Launch Vehicle - USA
Nova 8L - Launch Vehicle - USA
Nova 9L-1 - Rocket Stage - USA - Lox/Kerosene - 2,721,000 kg
Nova 9L-2 - Rocket Stage - USA - Lox/Kerosene - 1,814,000 kg
Nova 9L-3 - Rocket Stage - USA - Lox/LH2 - 363,000 kg
Nova 9L-4 - Rocket Stage - USA - Lox/LH2 - 118,000 kg
Nova 9L - Launch Vehicle - USA
Nova A-1 - Rocket Stage - USA - Lox/Kerosene - 1,342,000 kg
Nova A-2 - Rocket Stage - USA - Lox/LH2 - 403,000 kg
Nova A-3 - Rocket Stage - USA - Lox/LH2 - 40,000 kg
Nova A - Launch Vehicle - USA
Nova B-1 - Rocket Stage - USA - Lox/Kerosene - 1,995,000 kg
Nova B-2 - Rocket Stage - USA - Lox/LH2 - 614,000 kg
Nova B-3 - Rocket Stage - USA - Lox/LH2 - 63,000 kg
Nova B - Launch Vehicle - USA
Nova C-3 - Rocket Stage - USA - Nuclear/LH2 - 61,000 kg
Nova C - Launch Vehicle - USA
Nova D-3 - Rocket Stage - USA - Nuclear/LH2 - 96,000 kg
Nova DAC 2-1 - Rocket Stage - USA - Lox/LH2 - 4,943,000 kg
Nova DAC 2-2 - Rocket Stage - USA - Lox/LH2 - 1,633,000 kg
Nova DAC ISI-1 - Rocket Stage - USA - Lox/LH2 - 3,084,000 kg
Nova DAC ISI-2 - Rocket Stage - USA - Lox/LH2 - 1,696,000 kg
Nova DAC ISI - Launch Vehicle - USA
Nova DAC-1 - Rocket Stage - USA - Lox/Kerosene - 4,213,000 kg
Nova DAC-2 - Rocket Stage - USA - Lox/LH2 - 2,268,000 kg
Nova D - Launch Vehicle - USA
Nova GD-B-1 - Rocket Stage - USA - Lox/Kerosene - 9,070,000 kg
Nova GD-B-2 - Rocket Stage - USA - Lox/LH2 - 998,000 kg
Nova GD-B - Launch Vehicle - USA
Nova GD-E-1 - Rocket Stage - USA - Solid - 3,628,000 kg
Nova GD-E-2 - Rocket Stage - USA - Lox/LH2 - 4,535,000 kg
Nova GD-E - Launch Vehicle - USA
Nova GD-F-1 - Rocket Stage - USA - Lox/Kerosene - 9,977,000 kg
Nova GD-F-2 - Rocket Stage - USA - Lox/LH2 - 1,497,000 kg
Nova GD-F - Launch Vehicle - USA
Nova GD-H-0 - Rocket Stage - USA - Lox/LH2 - 295,000 kg
Nova GD-H-1 - Rocket Stage - USA - Lox/LH2 - 8,526,000 kg
Nova GD-H - Launch Vehicle - USA
Nova GD-J-1 - Rocket Stage - USA - Lox/Kerosene - 8,617,000 kg
Nova GD-J-2 - Rocket Stage - USA - Lox/LH2 - 1,270,000 kg
Nova GD-J - Launch Vehicle - USA
Nova MM 14A-1 - Rocket Stage - USA - Solid - 2,847,000 kg
Nova MM 14A-2 - Rocket Stage - USA - Lox/LH2 - 3,401,000 kg
Nova MM 14A - Launch Vehicle - USA
Nova MM 14B-1 - Rocket Stage - USA - Solid - 2,271,000 kg
Nova MM 14B-2 - Rocket Stage - USA - Lox/LH2 - 2,721,000 kg
Nova MM 14B - Launch Vehicle - USA
Nova MM 1B-1 - Rocket Stage - USA - Lox/Kerosene - 7,430,000 kg
Nova MM 1B-2 - Rocket Stage - USA - Lox/LH2 - 1,361,000 kg
Nova MM 1B - Launch Vehicle - USA
Nova MM 1C-1 - Rocket Stage - USA - Lox/Kerosene - 8,943,000 kg
Nova MM 1C-2 - Rocket Stage - USA - Lox/LH2 - 2,041,000 kg
Nova MM 1C - Launch Vehicle - USA
Nova MM 24G-1 - Rocket Stage - USA - Lox/LH2 - 5,040,000 kg
Nova MM 24G-2 - Rocket Stage - USA - Lox/LH2 - 1,043,000 kg
Nova MM 24G - Launch Vehicle - USA
Nova MM 33-1 - Rocket Stage - USA - Lox/LH2 - 10,489,000 kg
Nova MM 33 - Launch Vehicle - USA
Nova MM 34-0 - Rocket Stage - USA - Lox/LH2 - 227,000 kg
Nova MM 34-1 - Rocket Stage - USA - Lox/LH2 - 10,126,000 kg
Nova MM 34 - Launch Vehicle - USA
Nova MM R10E-2 - Launch Vehicle - USA
Nova MM R10E-2 - Rocket Stage - USA - Air/Lox/LH2 - 8,474,000 kg
Nova MM R10R-2 - Launch Vehicle - USA
Nova MM R10R-2 - Rocket Stage - USA - Air/Lox/LH2 - 8,647,000 kg
Nova MM S10E-1 - Launch Vehicle - USA
Nova MM S10E-1 - Rocket Stage - USA - Lox/LH2 - 10,317,000 kg
Nova MM S10E-2 - Launch Vehicle - USA
Nova MM S10E-2 - Rocket Stage - USA - Lox/LH2 - 10,302,000 kg
Nova MM S10R-1 - Launch Vehicle - USA
Nova MM S10R-1 - Rocket Stage - USA - Lox/LH2 - 10,470,000 kg
Nova MM S10R-2 - Launch Vehicle - USA
Nova MM S10R-2 - Rocket Stage - USA - Lox/LH2 - 10,502,000 kg
Nova MM T10EE-1-1 - Rocket Stage - USA - Lox/LH2 - 4,944,000 kg
Nova MM T10EE-1-2 - Rocket Stage - USA - Lox/LH2 - 1,125,000 kg
Nova MM T10EE-1 - Launch Vehicle - USA
Nova MM T10RE-1-1 - Rocket Stage - USA - Lox/LH2 - 4,979,000 kg
Nova MM T10RE-1 - Launch Vehicle - USA
Nova MM T10RR-2-1 - Rocket Stage - USA - Lox/LH2 - 9,089,000 kg
Nova MM T10RR-2-2 - Rocket Stage - USA - Lox/LH2 - 2,041,000 kg
Nova MM T10RR-2 - Launch Vehicle - USA
Nova MM T10RR-3-1 - Rocket Stage - USA - Lox/LH2 - 5,517,000 kg
Nova MM T10RR-3-2 - Rocket Stage - USA - Lox/LH2 - 1,229,000 kg
Nova MM T10RR-3 - Launch Vehicle - USA
Nova NASA-1 - Rocket Stage - USA - Lox/Kerosene - 2,268,000 kg
Nova NASA-2 - Rocket Stage - USA - Lox/Kerosene - 499,000 kg
Nova NASA-3 - Rocket Stage - USA - Lox/LH2 - 227,000 kg
Nova NASA - Launch Vehicle - USA
Nova Solid 4 - Rocket Stage - USA - Solid - 816,000 kg
Nova Solid 6 - Rocket Stage - USA - Solid - 1,224,000 kg
Nova-1 DAC - Launch Vehicle - USA
Nova-2 DAC - Launch Vehicle - USA
Nova - Spacecraft - Navigation - - USA
Nova - Launch Vehicle Family
Nowak - Lisa Marie Caputo Nowak - American Astronaut - 1996 NASA Group
NPG - Spacecraft - Manned - Space Station - USSR
NPS-2 - Rocket Engine - - Nuclear/LH2 propellants - kgf
NRL ELINT - Spacecraft - ELINT - - USA
NTS - Spacecraft - Technology - Navigation - USA
Nuclear 12 Gw - Rocket Engine - USA - Nuclear/LH2 propellants - 295,000 kgf
Nuclear 14 Gw - Rocket Engine - USA - Nuclear/LH2 propellants - 340,000 kgf
NUSAT - Spacecraft - Calibration - - USA
Nyberg - Karen L Nyberg - American Astronaut - 2000 NASA Group 18
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Last update 3 May 2001.
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© Mark Wade, 2001 .