Flight Atlas Logo
Flight Atlas
Follow me onX LogoLogin / Sign upSubscribe
Flight Atlas Logo
Flight Atlas
Follow me onX LogoLogin / Sign up
Subscribe
Flight Atlas Logo
Flight Atlas
X LogoLogin / Sign up
HomeLaunch HistoryRocket EncyclopediaFuture LaunchesStatistics & ChartsDashboard

Delta family

Delta II 6920-8

United States1990
Drawing of the Delta II 6920-8

A two-stage Delta II flown once in 1990 to launch the LACE and RME military experiments.

Launches
1
Success rate
100%
0 failures
First flight
14 February 1990
LACE & RME
Builder
McDonnell Douglas
Height
39 m
Diameter
2.4 m
Stages
2
Boosters
9 × Castor 4A
Propellants
Solid, Kerosene / LOX, Aerozine 50 / N2O4
Payload to LEO
3,983 kg

Launches per year

Delta II 6920-8
Other Delta rockets
Show as table
YearLaunchesDelta II 6920-8
197250
197360
197470
1975120
197690
1977100
1978100
197930
198030
198150
198270
198380
198440
198620
198720
198810
198980
1990111
199150
1992110
199370
199430
199530
1996100
1997110
1998130
1999110
200070
200170
200240
200390
200480
200530
200690
200790
200850
2009110
201040
201160
201240
201330
201450
201530
201640
201720
201830
201930
202010
202110
202210
202310
202410

Delta rockets

RocketFlownLaunchesSuccess rateHeightPayload to LEO
Delta 090019722100%34 m1,300 kg
Delta 16041972 to 19732100%35 m600 kg
Delta 03001972 to 1973367%34 m820 kg
Delta 19141972 to 19732100%35 m1,835 kg
Delta 191319731100%35 m1,835 kg
Delta 190019731100%35 m1,800 kg
Delta 23131974 to 1977367%35 m500 kg
Delta 29141974 to 19793093%35 m724 kg
Delta 23101974 to 19813100%35 m1,882 kg
Delta 29101975 to 19786100%35 m1,882 kg
Delta 141019751100%35 m350 kg
Delta 191019751100%35 m1,835 kg
Delta 29131975 to 19762100%35 m2,000 kg
Delta 39141975 to 19861283%35 m951 kg
Delta 39101980 to 19883100%35 m
Delta 3910/PAM1980 to 19827100%35 m1,087 kg
Delta 3913198110%35 m2,480 kg
Delta 39201982 to 19863100%36 m
Delta 3920/PAM1982 to 19876100%36 m1,280 kg
Delta 39241982 to 19875100%36 m2,385 kg
Delta II 69251989 to 199213100%38.1 m3,981 kg
Delta 3920-819891100%36 m2,480 kg
Delta 4925-81989 to 19902100%34 m3,400 kg
Delta 5920-819891100%34 m3,848 kg
Delta II 6920-819901100%39 m3,983 kg
Delta II 6925-819901100%39 m1,500 kg
Delta II 6920-101990 to 19922100%39 m3,950 kg
Delta II 79251990 to 20093694%38.9 m4,600 kg
Delta II 7925-81994 to 19962100%38.2 m4,550 kg
Delta II 7925-101994 to 19962100%38.9 m4,498 kg
Delta II 7920-101995 to 20179100%38.7 m5,959 kg
Delta II 7920-10C1997 to 201117100%38.7 m5,959 kg
Delta II 7920-819971100%39 m5,000 kg
Delta II 7925-9.51998 to 200926100%38.9 m4,600 kg
Delta II 7420-10C1998 to 201814100%38.7 m3,099 kg
Delta III 89301998 to 2000333%39.1 m8,290 kg
Delta II 7326-9.51998 to 20013100%38.4 m2,430 kg
Delta II 7425-9.51998 to 20023100%39 m2,880 kg
Delta II 7426-9.519991100%39 m2,870 kg
Delta II 73201999 to 20116100%38.9 m2,800 kg
Delta II 7425-1020011100%39 m2,886 kg
Delta II 7920-10L2002 to 20042100%40 m4,805 kg
Delta IV M+(4,2)2002 to 201915100%66.2 m11,920 kg
Delta IV M2003 to 20063100%63 m8,600 kg
Delta II 7925H-9.52003 to 20073100%38.9 m5,475 kg
Delta II 7920H20031100%38.9 m5,959 kg
Delta II 7320-10C2004 to 20156100%38.9 m2,800 kg
Delta IV Heavy2004 to 20241694%72 m28,370 kg
Delta II 7925-10L2006 to 20092100%38.9 m4,600 kg
Delta II 7925-10C20071100%38.9 m4,520 kg
Delta II 7920H-10C2008 to 20112100%38.9 m5,959 kg
Delta IV M+(5,4)2009 to 20198100%70.7 m13,730 kg
Delta IV M+(5,2)2012 to 20183100%72 m11,700 kg