# Grob G102 Astir

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German single-seat glider, 1974

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G102 Astir Astir CS in flight General information Type Club Class sailplane National origin Germany Manufacturer Grob Aircraft Designer Burkhart Grob Number built 1241+ History Introduction date 1975 First flight December 1974

Grob G 102 Standard Astir III N17999, National Air and Space Museum

The **G102 Astir** is a single-seat [glassfibre](/source/Glassfibre) [Club Class](/source/FAI_Club_Class) [sailplane](/source/Glider_(sailplane)), designed by [Burkhart Grob](/source/Burkhart_Grob) and built by [Grob Aircraft](/source/Grob_Aircraft). It was the first Grob-designed sailplane, with the first flight in December 1974. Grob had previously built the [Schempp-Hirth Standard Cirrus](/source/Schempp-Hirth_Standard_Cirrus) under licence.

## Design and development

The Astir CS [Club Standard] is of composite (fiberglass/resin) construction, has a large wing area, a T-tail and water ballast tanks in its wings. The large wing area gives good low-speed handling characteristics but its high-speed performance is inferior to other [Standard Class](/source/Glider_competition_classes#Standard_Class) gliders. In early versions, some of the fuselage frame was wood but this was replaced with a light alloy casting which sometimes cracked after heavy landings. The tail dolly is unusual by being a loose fit into a vertical hole and able to fall free if take-off is attempted with the dolly in place.

A slightly improved Standard Class version, the CS 77, was introduced in 1977. It has a different rudder profile and a slimmer fuselage similar to that of the Speed Astir. The Standard II and Standard III versions followed in the early 1980s, reverting to the higher-profile fuselage and with a reduced empty weight and an increased payload.

The Astir CS Jeans was similar to the CS 77, but had a fixed mainwheel and a tailskid. Its cockpit was fitted in blue denim. Later versions were the Club II and the Club III which also had fixed gear, but the Club III had a tailwheel.

The numbers built of each type were: 536 CS, 244 CS77, 248 CS Jeans, 61 Club/Standard Astir II and 152 Club/Standard Astir III. A flapped version called the [G104 Speed Astir](/source/Grob_G_104_Speed_Astir) was also produced.

The latest in the Astir line is the **G102 Standard Astir III**, designed by [Burkhart Grob](/source/Burkhart_Grob) and built by [Grob Aircraft](/source/Grob_Aircraft) as a development of the original G-102.

One Astir (now residing at the Steven F. Udvar-Hazy Center), flown by Robert Harris, broke the world absolute altitude record at 49,009 ft (14,938 m) on 17 February 1986. This record lasted until 2006.[1]

G102 Standard Astir III

G102 Astir of the Cape Gliding Club at Worcester airfield

Astir CS Jeans launching

## Variants

**Astir CS**
- The original production version of the Astir, produced up to 1977 (CS = Club Standard)

**Astir CS77**
- Production aircraft from 1977, with revised fuselage profile and other modifications

**Speed Astir**
- The Astir with a flapped wing to comply with the FAI 15m Flapped Class, for gliding competitions

**Astir CS Jeans**
- Astir aircraft with faired fixed undercarriage, to comply with the Club Class for gliding competitions and to provide "glass-ship" experience at lower cost.

**G102 Astir**
- Designation introduced by Grob for the Astir series in the 1980s, with each successive improvement given the suffix I, II or III etc.

**G104 Speed Astir**
- The Speed Astir re-designated

## Specifications (Standard Astir III)

*Data from* [Grob G102 manual](http://www.solidcad.hu/ass/GLIDING/LETOLTESEK_GLIDING/astir/grob102_flight_manual.pdf)

**General characteristics**

- **Crew:** 1

- **Length:** 6.75 m (22 ft 2 in)

- **Wingspan:** 15.0 m (49 ft 3 in)

- **Height:** 1.26 m (4 ft 2 in)

- **Wing area:** 12.4 m2 (133 sq ft)

- **[Aspect ratio](/source/Aspect_ratio_(aeronautics)):** 18.2

- **Empty weight:** 250 kg (551 lb) approximately

- **Gross weight:** 450 kg (992 lb) with water ballast; without ballast 350 kg (770 lb)

**Performance**

- **Maximum speed:** 170 km/h (110 mph, 92 kn) manoeuvring and airtow

- **Stall speed:** 59 km/h (37 mph, 32 kn) without airbrakes

- **[Never exceed speed](/source/V_speeds#VNE):** 250 km/h (160 mph, 130 kn)

- **Maximum glide ratio:** Best 38, at 105 km/h (64 mph, 56 kn) and 0.77 m/s (152 ft/m)

- **Rate of sink:** 0.62 m/s (122 ft/min) minimum, at 76 km/h (47 mph, 42 kn) and glide ratio 34

## See also

**Related development**

- [Grob G104 Speed Astir](/source/Grob_G104_Speed_Astir)

**Aircraft of comparable role, configuration, and era**

- [Glasflügel 205 Club Libelle](/source/Glasfl%C3%BCgel_205_Club_Libelle)

- [Schleicher ASK 23](/source/Schleicher_ASK_23)

- [SZD-51 Junior](/source/SZD-51_Junior)

**Related lists**

- [List of gliders](/source/List_of_gliders)

## References

Wikimedia Commons has media related to [Grob G 102 Astir](https://commons.wikimedia.org/wiki/Category:Grob_G_102_Astir).

- [Sailplane Directory](https://web.archive.org/web/20060926221015/http://www.sailplanedirectory.com/PlaneDetails.cfm?planeID=22)

- Hardy, M. *Gliders & Sailplanes of the World*. Ian Allan, 1982

- [Homepage of Grob Aircraft AG](https://www.grob-aircraft.com)

1. **[^](#cite_ref-1)** [List of official records](http://records.fai.org/gliding/current.asp?id1=275&id2=1) on the [Fédération Aéronautique Internationale](/source/F%C3%A9d%C3%A9ration_A%C3%A9ronautique_Internationale) web site[*[permanent dead link](https://en.wikipedia.org/wiki/Wikipedia:Link_rot)*]

v t e Grob aircraft G 102 G 103 G 103a G 103c G 104 G 109 G 110 G 112 G 115 G 116 G 118 G 120/TP G 140 G 180 GF 200 G 520 G 850

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Adapted from the Wikipedia article [Grob G102 Astir](https://en.wikipedia.org/wiki/Grob_G102_Astir) by Wikipedia contributors ([contributor history](https://en.wikipedia.org/wiki/Grob_G102_Astir?action=history)). Available under [Creative Commons Attribution-ShareAlike 4.0 International](https://creativecommons.org/licenses/by-sa/4.0/). Changes may have been made.
