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Minotaur vi, Payload accommodations, Performance – Orbital Minotaur VI User Manual

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Orbital Sciences Corporation

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Dulles, Virginia 20166

www.orbital.com

©2013 Orbital Sciences Corporation

BR10001_1610

Minotaur VI

Payload Accommodations

• Standard 2.34 m (92 in) diameter spacecraft fairing

• Optional 2.79 M (110 in) diameter spacecraft fairing

available

• Mission-specific fairing access doors for spacecraft support

• Spacecraft and fairing assembly integrated independently

from launch vehicle stages

• Well-defined launch environments derived from extensive

flight data

• Temperature, humidity and cleanliness control through

lift-off

• Standard 986 mm (38.81 in) diameter bolted interface with

optional spacecraft support options

- Single and multiple spacecraft adaptors

- Various flight-proven spacecraft separation systems

available, including low-shock designs

• Multiple Payload Adapter Fitting (MPAF) option

• Hydrazine upper stage for multiple orbit altitude capabilities

or increased orbital insertion accuracy

Orbit Altitude (km)

2600

2400

2200

2000

1800

1600

1400

1200

1000

800

Pa

yl

oa

d (

kg

)

200

400

600

800

1000

1200

1400

1600

1800

Performance

• System performance assured from extensive booster motor

flight history

• Cold gas attitude control system readily accommodates

a variety of spacecraft mission requirements, including
precise separation pointing and post-boost maneuvers

• Minotaur VI+ uses the optional STAR

37 upper stage to

provide up to 200 kg increased performance to LEO and
support for HEO missions with the following capability:

- 980 kg to MTO
- 860 kg to GTO
- 560 kg to TLI

63.4

°

72

°

90

°

SSO

Ø0.48 m

(19.2 in)

Ø0.61 m

(Ø24.2 in)

0.87 m

(34.5 in)

0.87 m

(34.5 in)

1.52 m

(60.0 in)

1.52 m

(60.0 in)

2.87 m

(113.3 in)

2.87 m

(113.3 in)

Ø2.51 m

(Ø99.0 in)

Ø2.05 m

(Ø80.9 in)

Ø38.81 in

Interface

(No Sep

System)

Ø38.81 in

Interface

(No Sep

System)

Fairing Sep Plane

Fairing Sep Plane

Ø1.68 m

(Ø66.3 in)

Ø1.33 m

(Ø52.5 in)

Standard Fairing

Optional Large Fairing

Copies of the Minotaur User's Guide

can be downloaded from:

www.orbital.com

Additional information should be obtained

from the USAF OSP Office

USAF SMC Space Development
and Test Directorate (SMC/SD)

Launch Systems Division (SMC/SDL)
Kirtland AFB, NM 87117-5778
(505) 853-5533 (505) 853-0507

For technical details or questions

please contact Orbital at:

[email protected]