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Spaceflight Crew Register
Training & Mission Fatalities
Spaceflight Chronology
wdt_ID ID Y M D Country Project Vehicle Reference Result Launch Site Altitude Peak Rocket Mass Payload Mass Launch Mass Lives Payload Identity A Class A Objective A Altitude A Mass A Payload Identity B Class B Objective B Altitude B Mass B Payload Identity C Class C Objective C Altitude C Mass C Payload Identity D Class D Objective D Altitude D Mass D Payload Identity E Class E Objective E Altitude E Mass E Crewmember 1 Crewmember 2 Crewmember 3 Crewmember 4 Crewmember 5 Crewmember 6 Crewmember 7 Crewmember 8 Crewmember 9
1 1 1957 Jan 26 USA Test for Thor-DM-18 Thor-DM-18 Thor-101 Failure Cape Canaveral Air Force Station, Florida 0.00 49,340.00 0 49,340.00 - 0.00
2 2 1957 Mar 1 USA Test for Jupiter-SM-78 Jupiter-SM-78 AM-1A Failure Cape Canaveral Air Force Station, Florida 14.00 49,800.00 0 49,800.00 - 14.00
3 3 1957 Apr 20 USA Test for Thor-DM-18 Thor-DM-18 Thor-102 Failure Cape Canaveral Air Force Station, Florida 0.00 49,340.00 0 49,340.00 - 0.00
4 4 1957 Apr 26 USA Test for Jupiter-SM-78 Jupiter-SM-78 AM-1B Failure Cape Canaveral Air Force Station, Florida 18.29 49,800.00 0 49,800.00 - 18.29
5 5 1957 May 1 USA Vanguard 1 Vanguard TV-1 Success Cape Canaveral Air Force Station, Florida 195.00 10,078.00 1.47 10,079.47 - Vanguard 1 Satellite Navigation 195.00 1.47
6 6 1957 May 15 USSR Test for R7-Semyorka-8K71 R7-Semyorka-8K71 M1-5 Failure Baikonur Cosmodrome, Tyuratam 100.00 84,694.77 0 84,694.77 - 100.00
7 7 1957 May 22 USA Test for Thor-DM-18 Thor-DM-18 Thor-103 Failure Cape Canaveral Air Force Station, Florida 0.00 49,340.00 0 49,340.00 - 0.00
8 8 1957 May 31 USA Test for Jupiter-SM-78 Jupiter-SM-78 AM-1 Success Cape Canaveral Air Force Station, Florida 500.00 49,800.00 0 49,800.00 - 500.00
9 9 1957 Jun 11 USA Test for Atlas-A Atlas-A 4A Failure Cape Canaveral Air Force Station, Florida 3.00 81,647.00 0 81,647.00 - 3.00
10 10 1957 Jul 12 USSR Test for R7-Semyorka-8K71 R7-Semyorka-8K71 M1-7 Failure Baikonur Cosmodrome, Tyuratam 20.00 84,694.77 0 84,694.77 - 20.00
Launch Vehicles

Launch Vehicles
Rocket Engines
wdt_ID id Engine AKA Manufacturer Country Propellant Name Oxidiser & Fuel Chambers Chamber Pressure Nozzle Diameter, Initial Nozzle Diameter Exit Nozzle Expansion Ratio Engine Weight Vacuum Thrust V Thrust Weight Ratio Sea Level Thrust SL Thrust Weight Ratio
1 1 AJ-10-37 - Aerojet Rocketdyne USA RFNA-UDMH Liquid, Liquid 1 700 0.128'0.128 0.810'0.810 40 : 1 90.00 37.677'37.677 42.69 33.800'33.800 38.29
2 2 AJ-10-41 - Aerojet Rocketdyne USA RFNA-UDMH Liquid, Liquid 1 700 0.128'0.128 0.810'0.810 40 : 1 1,884.00 38.671'38.671 2.09 34.692'34.692 1.88
3 3 AJ-10-42 - Aerojet Rocketdyne USA RFNA-UDMH Liquid, Liquid 1 700 0.128'0.128 0.810'0.810 40 : 1 1,884.00 38.671'38.671 2.09 34.692'34.692 1.88
4 4 AJ-10-101 - Aerojet Rocketdyne USA RFNA-UDMH Liquid, Liquid 1 700 0.132'0.132 0.810'0.810 37.52 : 1 90.00 34.300'34.300 38.86 30.500'30.500 34.56
5 5 AJ-10-104 - Aerojet Rocketdyne USA RFNA-UDMH Liquid, Liquid 1 700 0.221'0.221 1.400'1.400 40 : 1 90.00 35.088'35.088 39.75 34.694'34.694 39.31
6 6 AJ-10-104D - Aerojet Rocketdyne USA RFNA-UDMH Liquid, Liquid 1 700 0.221'0.221 1.400'1.400 40 : 1 90.00 37.000'37.000 41.92 36.584'36.584 41.45
7 7 AJ-10-118 - Aerojet Rocketdyne USA RFNA-UDMH Liquid, Liquid 1 700 0.133'0.133 0.840'0.840 40 : 1 90.00 34.184'34.184 38.73 33.800'33.800 38.29
8 8 AJ-10-118D - Aerojet Rocketdyne USA RFNA-UDMH Liquid, Liquid 1 700 0.133'0.133 0.840'0.840 40 : 1 90.00 34.083'34.083 38.62 33.700'33.700 38.18
9 9 AJ-10-118E - Aerojet Rocketdyne USA RFNA-UDMH Liquid, Liquid 1 700 0.221'0.221 1.400'1.400 40 : 1 90.00 35.100'35.100 39.77 34.705'34.705 39.32
10 10 AJ-10-118F - Aerojet Rocketdyne USA RFNA-UDMH Liquid, Liquid 1 896 0.221'0.221 1.400'1.400 40 : 1 95.00 41.871'41.871 44.94 41.400'41.400 44.44
Launch Facilities
wdt_ID ID Launch Site OP from OP to Continent Country Country Code Location Latitude Longitude
1 1 DZA-Ham.lc 1947 1967 Africa Algeria DZA Hammaguira, French Special Weapons Test Centre 31° 5'58.24" N 2° 50'8.92" W
2 2 DZA-Reg.lc 1961 1965 Africa Algeria DZA Reggane, French nuclear tests 26° 43'8.22" N 0° 16'36.88" E
3 3 COD-Sha.lc 1977 1978 Africa Congo, Democratic Republic COD Shaba North, Kapani Tonneo OTRAG Launch Center 7° 55'33.13" S 28° 31'39.58" E
4 4 EGY-Jab.lc 1957 today Africa Egypt EGY Jabal Hamzah ballistic missile test and launch facility 30° 7'32.70" N 30° 36'18.50" E
5 5 KEN-Bro.lc 1964 1988 Africa Kenya KEN Broglio Space Centre, Malindi, San Marco Platform 2° 56'26.88" S 40° 12'48.24" E
6 6 LBY-Taw.lc 1981 1982 Africa Libya LBY Tawiwa, Sabha, OTRAG Launch Center 26° 59'38.11" N 14° 27'51.30" E
7 7 MRT-Nou.lc 1973 1973 Africa Mauritania MRT Nouadhibou 20° 55'42.82" N 17° 1'53.51" W
8 8 ZAF-Ove.lc 1989 1990 Africa South Africa ZAF Overberg, Test Centre 34° 36'9.54" S 20° 18'8.93" E
9 9 CHN-Lao.lc 1960 1960 Asia China CHN Laogang, Shanghai Shi, Zhongguo 31° 01'83.00" N 121° 89'59.00" E
10 10 CHN-Shi.lc 1960 1966 Asia China CHN Shijiedu, Guangde, Base 603, Chinese Academy of Sciences 30° 56'14.75" N 119° 12'20.70" E
wdt_ID ID Class Propellant Formula (Complete) Oxidiser State Oxidiser Name Oxidiser Molar Mass Oxidiser Formula Mixture Ratio Fuel State Fuel Name Fuel Molar Mass Fuel Formula
1 1 AP AP-CTPB-Al Solid Ammonium Perchlorate 117.489'06 NH_4 ClO_4 2.33: 1 Solid CTPB (14%) Aluminium (16%) 3,301.988'01 14%(CTPB) + 16%(Al)
2 2 AP AP-HTPB-Al Solid Ammonium Perchlorate 117.489'06 NH_4 ClO_4 2.13: 1 Solid HTPB (12%) Aluminium (20%) 3,245.967'59 12%(HTPB) + 20%(Al)
3 3 AP AP-PBAN-Al Solid Ammonium Perchlorate 117.489'06 NH_4 ClO_4 2.13: 1 Solid PBAN (12%) Aluminium (20%) 206.200'54 12%(HTPB) + 20%(Al)
4 4 AP AP-PBAN-Al-Fe Solid Ammonium Perchlorate 117.489'06 NH_4 ClO_4 2.13: 1 Solid PBAN (12.04%) Aluminium (16%) Iron Oxide (0.4%) 206.200'54 12%(HTPB) + 20%(Al) + 0.4%(Fe O_2)
5 5 CF CF-Ammonia Liquid Chlorine Pentafluoride 130.445'02 ClF_5 3.56: 1 Liquid Ammonia (Azane) 17.030'52 NH_3
6 6 CF CF-Ethanol-72 Liquid Chlorine Pentafluoride 130.445'02 ClF_5 2.76: 1 Liquid Ethanol (72%) Water (28%) 37.205'62 72%(C_2 H_5 O) + 28%(H_2 O)
7 7 CF CF-Hydrazine Liquid Chlorine Pentafluoride 130.445'02 ClF_5 2.12: 1 Liquid Tetrahydridodinitrogen 32.045'16 N_2 H_4
8 8 CF CF-Hydrogen Liquid Chlorine Pentafluoride 130.445'02 ClF_5 9.00: 1 Liquid Hydrogen 2.015'88 H_2
9 9 CF CF-Methanol Liquid Chlorine Pentafluoride 130.445'02 ClF_5 2.71: 1 Liquid Methyl Alcohol 32.041'86 CH_3 OH
10 10 CFPF CFPF-Aerozine-25 Liquid Chlorine Pentafluoride + Perchloryl Fluoride 122.326'35 71%(ClF_5) + 29%(ClO_3 F) 2.96: 1 Liquid Hydrazine (25%) UDMH (75%) 53.085'12 25%(N_2 H_4) + 75%(C_2 H_8 N_2)
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