Star (rocket stage)
Star 37

Star (rocket stage)

Section Title: Star 37
Table Section Text: None

Name (Thiokol#)	Mass (kg)	Prop. mass fract.	Prop.	Casing	Thrust, vac. (kN)	Imp.	Burn (s)	Diam. (m)	Length (m)	Remark

Total	Empty	Spec., Isp (s)	Tot. (kNs)

Star-37 (TE-M-364-1)	621.2	62.7	558.4	0.899	Solid	?	43.50	260.0	1584.46	42	0.93	0.80

Star-37B (TE-M-364-2)	718.4	64.7	653.7	0.910	Solid	?	?	291.0	1858.91	?	0.93	?

Star-37C (TE-M-364-18)	1047.5	82.8	964.7	0.921	Solid	?	?	285.5	2707.19	?	0.93	?

Star-37D (TE-M-364-3)	718.4	64.7	653.7	0.910	Solid	?	?	266.0	1858.91	?	0.93	?

Star-37E (TE-M-364-4)	1122.7	83.1	1039.6	0.926	Solid	?	?	283.6	2910.03	?	0.93	?	Discontinued

Star-37F (TE-M-364-19)	934.1	67.3	866.8	0.928	Solid	?	?	286.0	2444.46	?	0.93	?	Discontinued

Star-37FM (TE-M-783)	1147.4	81.5	1065.9	0.929	HTPB	Titanium	47.26	289.8	3051.35	63	0.93	1.69	Developed and qualified for use as an apogee kick motor on FLTSATCOM

Star-37G (TE-M-364-11)	1152.4	86.4	1065.9	0.925	Solid	?	?	289.9	2988.36	?	0.93	?

Star-37N (TE-M-364-14)	622.9	63.5	559.3	0.898	Solid	?	?	290.0	1590.24	?	0.93	?

Star-37S (TE-M-364-15)	711.4	53.4	658.0	0.925	Solid	?	?	287.3	1872.43	?	0.93	?

Star-37X (TE-M-714-1)	1150.0	82.8	1067.2	0.928	Solid	Titanium	51.10	295.6	3047.69	60	0.93	?

Star-37XE (TE-M-714-4)	?	?	?	?	Solid	Titanium	?	?	?	?	0.93	?

Star-37XF (TE-M-714-6)	953.2	67.7	885.4	0.929	Solid	Titanium	?	290.0	2542.03	?	0.93	?

Star-37XF (TE-M-714-8)	882.5	67.1	815.4	0.924	Solid	Titanium	?	291.1	2342.74	?	0.93	?

Star-37XFP (TE-M-714-17/18)	955.3	71.7	883.6	0.925	HTPB	Titanium	38.03	290.0	2537.49	67	0.93	1.50	Qualified as the orbit insertion motor for Boeing's Global Positioning Satellite (GPS), and as the apogee motor for the RCA SATCOM Ku-Band satellite.

Star-37Y (TE-M-714-2)	1152.1	80.6	1071.4	0.930	Solid	Titanium	?	297.0	3118.20	?	0.93	?

Sentence(s)

Star-37FM (TE-M-783) is a HTPB model used for FLTSATCOM.

final_sentence: Star-37FM (TE-M-783) is a HTPB model used for FLTSATCOM.